Pershing 1a Field Service Data Notebook

(

PERSHING la FIELD SERVICE DATA NOTEBOOK he Fi eld Service Data Notebook is cha nged as fol lows:

1. The attached new pages, as enumerated be low, wi ll be inserted in the ma nua l and the old pages _,1ill be removed. New or c hanged material in t he se pages is indicated by a vertical line in the margin of the page or by the FSNB or Ml number of t he illustrations. Extensively changed or added ch ap•ers , tables, etc, are indicated by a vertical line by '-fhe title only. Remove pages

I nsert pages

l ·l l ·3, 1·4 1·4.111·4.2 1·5 t hru 1-8 1·8. 1 thru1-8.4 1·9, 1· 10 2·3 thru 2•8 2· 13, 2-14 4 -1 thru 4-8.2 4·9 thru 4· 12. 4 4· 15 thru 4- 18 4·2 1, 4·22 4·25 t hru 4-28 4-3 1, 4·32 5·3, 5.4 6·3, 6-4 7·l 7-3, 7.4 9· 1, 9·2 9·9 thru 9·14 9.49

1·1 11·2 l ·3, l ·4 l ·4. 111 ·4.2 1·5 t hru 1·8 l ·8. 1 th ru l ·8.4 1·9 t hru 1· 10.2 2·3 thru 2-8 2· 13, 2· 14 4·1 thru 4-8 4 -9 th ru 4-12.6 4-15 t hru 4·18 4-2 1, 4-22 4·25 t hru 4·28 4·31. 4-32 5·3, 5.4 6-3, 6-4 7·1 th ru 7-2.2 7-3, 7.4 9·1 , 9· 2 9-9 thru 9· 14 9·49, 9·50

C4, 30 September 1972

,.

Remove pages

Insert pages

None

9-51 th ru 9-58 10-1/1 0-2 10-9, 10-10

10-1 10-9, 10-10 10-10.1 10-11thru10-16.2 10-17thru 10-21 11-5, 11 -6 14-5, 14 -6 15-27, 15-28 15-31, 15-32

None

10-11thru10-16 10-17, 10-18 11 -5, 11-6 14-5, 14-6 15-27, 15-28 15-3 1, 15-32

2. Retain the tra nsm ittal sheet in the fro nt of the manual for future reference.

C4

CHAPTER 1 SYSTEM (CONTENTS) Item Commonly used abbreviations ........... . Firing position ...................................... Firing position cabling diagram ................................ ............ . Firing site torque values ...................... Misfire ................................................. . Nomenclature cross-reference .......... . Safety considerations ......................... . Typical QRA position of equipment for alert readiness status ................ .

C4

Reference

Page

Ta ble 1-3 Fig. 1-1

1-10 1-8. 1

Fig. 1-1.1 Table 1-2 Par. 1-2 Table 1-1 Par. 1-1

1-8.2 1-7 1-4 1-4.1 1- 3

Fig. 1-2

1-9

1-1/ (1·2 blank)

I

PERSHING la FIELD SERVICE DATA NOTEBOOK

The Field Service Data Notebook 1s changed as follows: 1. The attached new pages, as enumerated be-

low. will be inserted in the manual and the old pages will be removed. New or changed material in these pages is indicated by a vertical line in the margin of the page or by the FSNB or MI number of the illustrations. Extensively changed or added chapters, tables, etc, are indicated by a vertical line by the title only.

Remove pages

Insert pages

i, ii 1-3. 1-4 1-4.1 1-5, 1-6 1-8.1 thru 1-8.3 1-13 2-3. 2-4 2-7. 2-8 2-13, 2-14 3-3 thru 3-8 4-7. 4-8

i, ii 1-3, 1-4 1-4.1/ 1-4.2 1-5, 1-6 1-8.1 thru 1-8.4 1-13/ 1-14 2-3, 2-4 2-7' 2-8 2-13, 2-14 3-3 thru 3-8 4-7, 4-8 4-8.1/ 4-8.2 4-12.3/ 4-12.4 4-13, 4-14 4-14.1, 4-14.2 4-31 thru 4-36 5-3 t hru 5-6 7-7, 7-8 8-3 t hru 8-6 9-11 . 9-12 9-29. 9-30

None None 4-13. 4-14 4-14.1 4-31 thru 4-36 5-3 thru 5-6 7-7. 7-8 8-3 thru 8-6 9-11. 9-12 9-29. 9-30

C3, 30 AUGUST 1971

Remove pages

10-5 thru 10-10 10-15, 10-16 None 10-17 thru 10-20 12-3, 12-4 13-3 thru 13-8 14-3 thru 14-8 None 15-3, 15-4 15-13, 15-14

Insert pages

10-5 thru 10-10 10-15, 10-16 10-16.1/10-16.2 10-17 thru 10-20 12-3, 12-4 13-3 thru 13-8 14-3 thru 14-8 14-8.1/14-8.2 15-3, 15-4 15-13, 15-14

2. Retain the transmittal sheet in the front of the manual for future reference.

C3

PERSHING 1a FIELD SERVICE DATA NOTEBOOK

The Field Service Data Notebook 1s changed as follows: 1. The attached new pages, as enumerated below, will be inserted in the manual and the old pages will be removed. New or changed material in these pages is indicated by a vertical line in the margin of the page or by the FSNB or MI number of the illustrations. Extensively changed or added chapters, tables, etc, are indicated by a vertical line by the title only. Remove pages

i, ii 1-3, 1-4 1-4.1 1-5 thru 1-8 1-8.1 1-9, 1-10 1-13 2-9 thru 2-14 3-3 thru 3-8 4-1 4-3 thru 4-6 4-9, 4-10 4-14. l 4-15, 4-16 4-31, 4-32 4-35, 4-36 6-3,6-4 7-3 thru 7-8 9-5 thru 9-8 9-15, 9-16 9-19, 9-20 9-43 thru 9-46

C2, 4 September 1970

I naert pages

i, ii 1-3. 1-4 1-4.1 1-5 thru 1-8 1-8.1 thru 1-8.3 1-9, 1-10 1-13 2-9 thru 2-14 3-3 thru 3-8 4-1 4-3 thru 4-6 4-9, 4-10 4-14.1 4-15, 4-16 4-31, 4-32 4-35, 4-36 6-3. 6-4 7-3 thru 7-8 9-5 thru 9-8 9-15, 9-16 9-19, 9-20 9-43 thru 9-46

r

Remove pages

l nsert pages

10-1 10-5, 10-6 10-9, 10-10 10-11, 10-12 10-17 thru 10-20 11-3. 11-4 13-5, 13-6 None 13-7. 13-8

10-1 10-5. 10-6 10-9, 10-10 10-ll. 10-12 10-17 thru 10-20 ll-3. 11-4 13-5. 1'3-6 13-6.1 , 13-6.2 13-7, 13-8


C2

PERSHING 1a FIELD SERVICE DATA NOTEBOOK

The original issue of the Field Service Data Notebook is ch'anged as follows: 1. The attached new pages, as enumerated below, will be inserted in the manual and the old pages will be removed. New or changed material in these pages is indicated by a vertical ..Jine in the margin of the page or by the FSNB or MI number of the illustrations. Extensively changed or added chapters, tables, etc, are indicated by a vertical line by the title only. Remove pages

i , ii 1-3, 1-4

None 1-7, 1-8

None 1-9 thru 1-13 2-3, 2-4 2-9 thru 2-14 3-3 thru 3-8 4-5 thru 4-12

None 4-13, 4-14

None 4-15 thru 4-39 &-1 &-3 thru 5-6 6-3 thru 6-6 7-3 thru 7-8 8-3 thru 8-6

Cl, 17 APRIL 1970

Insert pages

i, ii 1-3, 1-4 1-4.1 1-7, 1-8 1-8.1 1-9 thru 1-13 2-3, 2-4 2-9 thru 2-14 3-3 thru 3-8 4-5 thru 4-12 4-12.1, 4-12.2 4-13, 4-14 4-14.1 4-15 thru 4-39 5-1 5-3 thru 5-7 6-3 thru 6-6 7-3 thru 7-8 8-3 thru 8-6

Remov e pages

Insert pages

9-1. 9-2 9-5, 9-6 9-9 thru 9-36 9-43 thru 9-48 10-1 10-3 thru 10-10 None 10-11 thru 10-14 10-17 thru 10-21 11-3 thru 11-6 12-3 thru 12-5 13-3 thru 13-6 13-9 14-3 thru 14-11

9-1, 9-2 9-5, 9-6 9-9 thru 9-36 9-43 t hru 9-49 10-1 10-3 t hru 10-10 10-10.l 10-11 thru 10-14 10-17 thru 10-21 11-3 thru 11-6 12-3 thru 12-5 13-3 thru 13-6 13-9 14-3 thru 14-10

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NOTE: EXPOSURE TIME LIMITS DO NOT APPLY WHEN TELEPHONE HEADSET IS WORN.

20 Fl

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PTS/PS VEHICLE WITH PROGRAMMER· TEST STATION AND POWER STATION MOUNTED

POWER SIAllON

DANGEROUS NOISE LEVEL EXISTS IN THE VICINITY OF AN OPERATING IRAl
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LEGEND: " ' ' ' I FOOT: 1/2 HOUR PER DAY 2 FEET: 3 HOURS PER DAY W.&«:i$ 4 FEET: NO WORK AREA (PASS THROUGH ONLYI Y//h 8 FEET: 4 HOURS PER DAY

PERMANENT EAR DAMAGE MAY RESULT IF PERSONNEL REMAIN EXPOSED TO NOISE BEYOND THE SAFE TIME LIMITATIONS WITHOUT ADEQUATE PROTECTION. THE NOISE EXPOSURE TIME LIMITS ASSIGNED TO VARIOUS WORK AREAS ARE AS ILLUSTRATED

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NOTICE The PERSHING la Field Service Data Notebook contains reference information and data pertinent to the PERSHING la Field Artillery Missile System. The material contained herein is not to be used in lieu of information, procedures, and technical data contained in Department of the ArmY. Technical Manuals. The tactical firing procedures containea..,.i in TM 9-1425-381-10 are to be used at all times during firing battery operations. Recommendations for changes or improvements should be submitted to: Martin Marietta Corp. ATTN: Chief, Pershing Logistics Engineering MP 486 P.O. Box 5837 Orlando, Fla. 32805

I

MARGIN INDEX

To use, bend outer edge of book backwards; then follow margin index of desired chapter to page with black edge marker.

Issued by the PERSHING Project Manager's Office, Redstone Arsenal, Alabama 35809, for informal use.

ii

C3

PERSHING la FIELD SERVICE

DATA NOTEBOOK Chapter

.......,

Page

1.

System ........................................... ......

1-1

2.

Missile, conta in ers, blankets, and hoisting beams....... ............ ..... ...........

2-1

3.

Erector-launcher... ................. ............ ....

3-1

4.

Programmer-test station .........................

4-1

5.

Power station .............. .......... ...... ..........

5- 1

6.

Azimuth layin g set .. ........................... ....

6-1

7.

Battery contro l centra l .... .. ......................

7·l

8.

Radio te rminal set.. .. ...... ............. ...........

8 ·1

9.

Cable data .... ...... .. ..... .... ............ ...........

9·l

10.

System components test station .... .. .........

10· l

11.

Shop sets.. ................ ............................

11 · l

12.

Power station equivalent.. ...... .. .. .. ...........

12-1

13.

Vehicles .... ..... .. .. ........ ........... ..... ..... .. ... .

13- 1

14.

Pu blicat ions ................................ .. ....... .

14· l

15.

Conversion tables ...... ... ........................ .

15-1

..,,,,,,

iii

II II Ill Ill II Ill Ill Ill Ill Ill II II II

II II

r

CHAPTER 1 SYSTEM (CONTENTS) Item Commonly used abbreviations .......... . Firing position ............................... .. Firi ng site torque values .................. . Misfire ................... ... ... .. ............ .... . Nomenclatu re cross-refer ence ........ .. Safety co nside rations ..................... .. Typical position of equipment for

QRA .... ............... .... ... ................. .

Reference Table Fig. Table Par. Table Par.

1·3 l ·l 1-2 1·2 l ·l 1-1

Fig. 1·2

Page 1-10 1-8

l ·7 1·3

1-4 1-3

1·9

1- 1

II

r

CHA PTER 1 SYST EM 1-1 . Safety Co nsiderations.

I

WARN ING

I

Do not apply full powe r sim ultaneously to two miss iles if t hey are posit ioned closer th an 55 meter s ( 180 feet) . a. Blast Area. To provide personnel safety from missile blast during fi ring. per · sonnel are evacuated to a position at least 150 meters (492 feet ) from the missile. Personnel are evacua ted as soon as the ir duties have been completed. The last man leaves the immedia te fi ring position approx imately 15 seconds before the FIRE swi tches are pressed; however, th e FIRE swi tches will no t be pressed until all pe rsonne l ha ve reached th e pro per distance. All loose or fl ammable items of equ ipme nt must be clea red f rom the initial blast area pri or to fi ri ng. The ini t ial bl ast area extends to eithe r side of t he blast deflector, and includes t ha t area within a 50 ° sector from t he center of the blast deflector out to a distance of 55 meters (180 feet ). b. Gen era l Preca ut ions. ( 1 ) Personn el must be fam iliar with and must ob· serve all sa fety precautions when wo r king on or ha nd lin g electronic equipment, high.press ure air systems, haza rdo us solve nts, and toxic an d fla mma ble chem ica ls . Fa ilure to observe safety precautions may result in death or sever e inj ury. ( 2 ) Pe rsonn el wit hin t he area du r ing prepa ration and fir ing of the m issil e will be lim ited to those necessa ry to accom plish the opera tion. ( 3) Dr illing equipmen t of any ty pe will not be us ed in th e modi fica tion of items con tain ing explosives. ( 4 ) For preca utions pertainin g to nuclea r war hea d operat ion s and han dling, refer to TM 9 · 1 100· 375·12.

C4

1-3

I

I

c. Pe rsonne l Safety During an Electrical Storm.

IWA RNING I Protect personnel from lightning. The missile on the EL is susceptible to lightn ing strikes. This threat is greatly increased when the missile is vertical. When the commander determines that the threat of an electrical storm is imminent, he will insure that the missile is lowered and personnel are cleared from the immediate vicinity of the equip· men! when such action will not interfere wi t h accomplishment of his mission.

I

c.l. Equipment Sa fety During an Electrical Storm .

I CAU~IO N I

Protect equipment from lightning. (1) The firi ng position equipment, especia lly in the standby configuration, i s vulnerable to lightning strikes. When the commander determines that the threat of an electrical storm is imminent, he will insure that cables 60W18, 60W105, and 60W109 are disconnected at both ends when such action will not interfere with his mission. (2) In order to resume alert readiness status withou t delay after the threat of elect rical storm passes, the commander will insure that all cables are connected and that missile conditioning is restored. d. Power Station Refueling. The power station, refueling pump, and hose nozzles must be grounded , and operable fire fighting equipment must be present du r ing fueling opera t ions.

1- 2. Misfire. A misfire condition exists when a tactica l missile fails to achieve lift-off after the FIRE switches are pressed the second time. A misfire occu rr ing before cable mast ejection 1s considered to be safe. A misfire occurring after cable mast ej ection is considered to be unsafe, since a haza rdous situation, such as motor explosion, may exist. If th e nor ma l seq uence of events does not occur after the FIRE switches are pressed on t he remote f iring box , the un it commander is notified immediately; then, as di-

1-4

C4

r

rected by the unit commander, the procedures prescribed " ' in TM 9-1425·381-10 are performed.

Table l · 1 • Nomenclature Cross-Reference Common

Official

AC generator set, or ac power trailer

Trailer Mounted Diesel Engine Generator Set PU ·614/M

Assembly tester

Electronic Circuit Plug-In Unit Test Set OQ-25/MSM-94

Azimuth laying container

Guided Missile Azimuth Laying Set Shipping and Storage Con· tainer XM521 and XM522

Azimuth laying control box or ALCB Azimuth laying set

Guided Missile Azimuth Orienta· tion Control Box C-7767 /G

Azimuth laying training set

Guided Missile Azimuth Laying Training Set XM79

Battery control central or BCC

Guided Missile Battery Control Central AN/MSW·8

Card and module test set or CMTS

Electronic Circuit Plug-In Unit Test Set TS-2604/TSM-87

Computer

Missile Programmer· Test Sta· tion Computer CP-988/TSM· 87

Countdown control panel assembly or CDCP

Missile Programmer- Test Sta· tion Countdown Control Unit AN/TSA-32

Cradle

Atomic Warhead Section Cradle H4211B-1

Crane pack lifting sling set

Multiple Leg Sling XM28

Erector-launcher 10-kw generator and spare wheel assembly mounting kit

Guided Missile EquipmentVehicle Accessory Kit XM219

C4

Guided Missile Azimuth Laying Set XM78

1·4.1/(1·4.2 blank)

I

r

Table 1-1 . Nomenclature CrossReference-Contin ued Common

I._/

l._,I

Official

Erector-launcher or EL

Guided Missile Semitrailer Mounted Erector-Launcher XM790

First and second stage cradle

Guided Missile XM12

First stage

Guided Missile Propulsion Sec· tion XMlOl

First stage blanket First stage container

Electrically Heated Guided Missile Section Blanket XM7 Guided Missile Propulsion Section Shipping and Storage Coo· tainer XM475

First stage hoisting beam

Guided Missile Hoisting Beam XM33

Guidance section blanket

Electrically Heated Guided Missile Section Blanket XM6

Guidance section container

Guided Missile Guidance Section Shipping and Storage Container XM474

Guidance section hoisting beam

Guided Missile Hoisting Beam XM32

Guidance section or GS

Guided Missile Guidance Section AN/DJW-28 or AN/DJW-35

Instant air cylinder and support rack assembly

Air Servicer, Guided Missile Gyroscope

Maintenance panel assembly or MP

Missile Programmer-Test Sta· tion Fault Locator AN/TSA-31

Missile

Surface Attack XMGM-31A

Section Cradle

Guided Missile

Mounting kit

Mounting Kit, Power Station

Pneumatic test console

Guided Missile Pneumatic Test Set AN/MSM-96

Power distribution set

Guided Missile System Power Dis· tribution Set AN/GSA-109 or AN/GSA-111

~

C3

1-5

I

Table 1-1 • Nomenclature CrossReference-Continued Official

Common

Power station equivalent or PSE

Trailer Mounted Guided Missile System Power Station AN/ MJQ-3

Power station or PS

Transportable Guided Missile System Power Station AN/T JQ-3

Programmer-test station or PTS

Transportable Guided Missile Programmer-Test Station AN/ TSM-87

Programmer-test station/power station mounting kit

Transportable Guided Missile Equipment Mounting Kit

Protector-sling

Atomic Warhead Section Protector-Sling H42l18-2

Radio terminal set and winterization heater mounting kit

Transportable Guided Missile Equipment Mounting Kit

Radio terminal set or RTS

Radio Terminal Set AN/TRC-80

Radio terminal set 10-kw generator mounting kit

Guided Missile Equipment Mount· ing Kit XM 184

SCTS

Semitrailer Mounted Guided Mis· sile System-System Components Test Station AN/MSM-94

SCTS van

6-Ton 2-Wheel Electronic Van Semitrailer 373A2

Second stage

Guided Missile Propulsion Section XM102

Second stage blanket

Electrically Heated Guided Missile Section Blanket XM9

Second stage container

Guided Missile Propulsion Section Shipping and Storage Container XM4 76

Second stage hoisting beam

Guided

Shelter

Electrical Equipment Shelter S· 367 /TSM-87

'

1-6

Missile

Hoisting Beam

XM33

C4

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Table 1-1. Nomenclature CrossReference-Continued Common

~

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Official

Shipping container sling

Multiple Leg Sling XM27

T-zero tactical simulator

T-Zero Tactical Simulator Guided Missile System Training Set

Tape reader

Punched Tape Reader MX-7874/ TSM-87

Trainer

Training Guided Missile XM-19

Warhead section or WS

Atomic Warhead Section XM28, XM141, or XM142

WS container

Atomic Warhead Section Shipping and Storage Container XM483

Table 1-2. Firing Site Torque Values Item

~

~

Torque

Air vanes

22 in.-lb

Air vanes (in container)

27 in.-lb

Azimuth ring clamp assembly screws

100 ft-lb (with missile); 18 ft-lb (without missile)

Azimuth ring clamp release mechanism (before ring clamp installation)

108 in.-lb

Azimuth ring clamp release mechanism (after ring clamp installation)

120 in.-lb

Connector adapter

Until adapter is seated firmly against connector shoulder, not exceeding 85 ft-lb torque.

C4

1-7

I

(

Table 1-2. Firing Site Torque Values-Continued Torque

Item Connector receptacle retaining nut Shell size 12 Shell size 16 Shell size 20

12 ft-lb 20 ft-lb 29 ft-lb

Container cover (WS)

47 ft-lb

Explosive bolt cartridges (detonators)

50 in.-lb

Forward and rear clamp ring (guidance section container)

17 ft-lb

Forward clamp ring bolts

25 ft-lb (1st stage conta in er); 17 ft-lb (2nd stage conta in er)

Initiators (1st and 2nd stages)

15 ft-lb

Jet vane retainer bolt

35 in.-lb

Rear clamp ring bolts (1st and 2nd stage containers)

50 ft-lb

I

Splice band nuts (2nd stage·to-guidance section)

45 ft-lb

I

Retaining ring nuts

50 ft-lb (with missile); 20 ft-lb (without missile)

I

Rocket motor port plugs

16 ft-lb

Shaped charge retainerassemblies (rear screws only)

10 in.-lb

I

Splice band nuts (1st stage· to-2nd stage)

45 ft-lb

I

Splice band nuts (guidance section-to-WS)

23 ft-lb (with warhead section): 10 ft-lb (without warhead section)

Warhead section support plate splice band bolt

55 in.-lb

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?010>0 tUIOtl

•

I

Figure 1-2. Typical QRA position of equipment in alert readiness status.

Cl

I 1-9

Table 1-3. Commonly Used Abbreviations

AA AC/DC DVM ACAS ACS ADJ ADV

ALCB ALCP AMPL AOL AOT AOU AUTO AUX B

BCC CAS

cc

CDCP CDP CE CFS CM CM CMA CMPNT CMTS CNM CORR CPE CR CRD CRV DEM OD

DIM DIR DIRAD DOM

DP DR DR EAC

EBW

EL 1-10

aiming azimuth ac/ de differential voltmeter assistant chief of ammunition section assistant chief of section adjust advance azimuth laying control box azimuth laying control panel amplifier altitude of launch altitude of target azimuth oriented unit automatic auxiliary signal bus battery control central chief of ammunition section capacitor module countdown control panel central data processor command element chief of firing section command module crewman cable mast assembly component card and module test set circuit network module correct circular probable error cross range cross range displacement cross range velocity demodulator data input multiplex data input register data input register to adder data output multiplex fuze decrement constant data register driver (vehicle) end around carry e~ploding bridgewire erector-launcher

C4

r Table 1-3. Commonly Used AbbreviationsContinued EMP

ENA ENC ENDIR

C4

electro-magnetic pulse enable A register enable C register enable data input register

1-10.1/(1·10.2 blank)

I

r-

Table 1-3 . Commonly Used Abbreviations-Continu ed

..,,,,

ENF ENP ENXL EOL EOT EXT FA FAM FAS FASV FC MON ITOR FDT FF FIL FS FSN GEN GNC GSR HEFU HEIS HLT HOB HPS Hz INTG INV INVR 1/0 IR IRI LA L LAT LAY LC LCP LOL LOT LPS LSB LSD LSH

Cl

enable F register enable program co unter enable index location register easting of launch ea sting of target exte rnal firing azimuth firing azimuth in mils fi eld alert status fi eld alert status verification frequency and constant monitor fac ilities distribution t ra iler flip- flop filtered firing section Federal stock numbe r generator grid north correction genera I support ro le high energy firing un it high energy initiate system horizontal laying theodolite height of burst high -pressure switch Hertz (cycles per second) integrator inverter inverter input/output input register information readout indicator latitude of launch latit ude of ta rget laying long coast launch control pa nel assembly longitude of launch longitude of target low-pressure switch least significant bit least significant digit least significant half

I

I

1- 11

Table 1-3 . Commonly Used Abbreviations-Continued M M MAM MB MCP MD MOE ME MEAS MH MM IMOD MON MP MSB MSD MSH NOL NOT NSG OIC OL OLT OP OP OR OST p

I

PC PDB PDS I PLATF PPS PR PS PSE PTS PVC PWR Q QD QRA R

1-12

monitor module multiplier consta nt memory address multiplex mea surement bus master control pane l matrix driver manual data entry monitor element measurement missile handler monitor module modulator monitor maintenance panel most significant bit most significant digit most significant ha If northing of launch northing of target north seeking gyro officer in charge orienting line orienting line target operation operator outp ut register orienting station theodolite program printed circuit power distribution box power distribution system platform programmab le power supp ly printer-receiver power sta tion power station equivalent programmer-test station programmable volta ge comparator powe r slant range velocity quick disconnect quick reaction a lert reset (relay)

Cl

r Table 1-3. Commonly Used Abbreviations-Continued

\.,,I

REF .REG RET RFB RFBB RFI RG RGZ RTS

~

SA SAD SAV SC SCR

I.._/

s

scs

SCTS SIM S/N SRO SRV SUB SUPV T TAT TEMP TFS

tHEOO TN

....,,., TP

TPRD UN REG UUT VK VLT

~

ws

WSS

C3

reference regulated return remote firing box remote firing box bus radio frequency interference range range beyond ground zero radio terminal set set (relay) slant altitude slant altitude displacement slant altitude velocity short coast silicon controlled rectifier silicon controlled switch system components test station simulate serial number slant range displacemefrt slant range velocity substitute command supervisor guidance cutoff coefficient target atmosphere tern pera t~ re thermal fuze battery ignition time theodolite test number test point tape reader u n regulated unit under test fuze reference velocity vertical laying theodolite warhead section warhead section simulator assembly

I

•

1-13/(1·14 blank)

;yr

~,,

"\

r

CHAPTER 2 MISSILE, CONTAINERS, BLANKETS, AND HOISTING BEAMS (CONTENTS)

....,

'..._)

Item

Reference

Page

MISSILE Missile section skin surface damage criteria, maximum limits ...............................•..... PERSHING missile ..•.•.•...•..•....... Surface damage criteria .•........... Warhead section ablative coating damagEt criteria, maximum limits ..•...•.•.............•.•....•.......

Table 2·1 Fig. 2-1 Par. 2-1

2-4 2-6 2-3

Table 2·2

2-5

Fig. 2·2

2-9

Fig. 2·4 Par. 2-3 Table 2·3

2-11 2-7 2-8

Fig. 2-3 Par. 2-2

2-10 2-7

Fig. 2-5

2-12

2·6 2-8 2-7 2-4 2-9

2-14 2-18 2-16 2-13 2-i9

Par. 2-5 Fig. 2-10

2-20 2-21

Fig. 2-11

2-22

CONTAINERS First stage shipping and storage container ............................... Guidance section shipping and storage container .................... Humidity indications .................. Relative humidity indications ....... Second stage shipping and storage container .................... Tabulated data .......................... Warhead section shipping and storage container ....................

"WI

~

BLANKETS First stage blanket ..................... Guidance section blanket ............ Second stage blanket ................. Use of blankets ......................... Warhead section blanket ............ HOISTING BEAMS Ancillary equipment tiedown kit. .. Hoisting beams .......................... Hoisting beam storage on wrecker M543 ........................

Fig. Fig. Fig. Par. Fig.

2·1

•

r

r CHAPTER 2 MISSILE, CONTAINERS, BLANKETS, AND HOISTING BEAMS MISSILE 2-1. Surface Damage Criteria.

1...J

a. General. This paragraph specifies the surface damage criteria for accepting or rejecting the first and second stages, the guidance section, and the warhead section. The depth of surface defects can be determined with a standard dial-indicating ·depth micrometer. The maximum depth limits for scratches and gouges listed below are based on the assumption that the surface finish in the damaged area has not been removed. If the finish is re· moved, the allowable depth is 0.003 inch less than speci· fied. This limitation does not apply to dents. Refer to TM 9-1100-375·12, TM 9-1410-375·34/l, and TM 9·1410-375·1 35 for additional damage criteria information. b. Definitions. ( 1) Crack. A partial fracture; when the part is not completely divided. ( 2) Dent. A slight depression; rounded hollow in a surface.

a small, smoothly

( 3) Gouge. Displacement of material from a surface, due to a cutting or tearing action. ( 4) Nick. A sharp indentation in a surface, especially on an edged part. ( 5) Open skin area. The area of skin surface that is not reinforced and is not between reinforcing rivets, spot welds, bolts, etc. ( 6) Reinforced skin area. The area of skin surface that is reinforced from within and is between the rein· forcing rivets, spot welds, bolts, etc. ( 7) Scrape.- A broad scratch; a shallow surface blemish. ( 8) Scratch. Narrow and shallow displacement of material from a surface.

C4

2-3

~

(")

.,..N

0 .014 0 .013 0.010

0 .012 0.010

7 -314 2 6

9·314 4

Open skin area 1

0 .021 0 .0 18

0.025 0.021 0.0 18

area '

Rein· for ced

1.00 0.100

0. 100 0.100 0.100

leng th (in.)

Nicks

0.021 0 .017

0 .025 0 .023 0 .018

Open skin area '

4.00 4.00 4.00

4.00 4.00

4.00 4.00

0 .039 0.033

' '

Width

4.00 4.00 4.00

l ength

0 .045 0.039 0 .035

Rein · forced area '

Depth (in.)

0.080 0.072

0.080 0.080 0.063

Depth

Dents'

0.030 0 .030

0.030 0.030 0 .030

Slope rate

Max i mum of two scratches or gouges in any 8-inch square. No two den t s having a depth grea ter than 0.020 inch may be with in 10 inches of adjacent edges. Not more than four dent s having a depth greater than 0.010 but less than 0.020 inch may be contained in any 8-inch square. Any dent having a depth greater than 0.020 inch will be dye penetrant tested for surface cracks. Presence of surface cracks is cause for rejection.

' If the fini sh is removed. the allowable dept h i s 0.003 inc h less t han specified.

First stage: Aft body section Forward ski rt Guidance section (all surfaces) Second stage: Aft body section Forward skirt

Item '

len gth (in .)

Depth (in.)

Scratches and gouges'

Table 2-1. Missile Section Skin Surface Damage Criteria, Maximum Limits

I

r

Table 2-2. Warhead Section Ablative Coating Damage Criteria, Maximum Limits Chips, scratches, dents Length (in.)

Depth (in.)

Area (sq in.)

Forward surface (nose cone)

3

0.030

0.25

Aft area

6

0.062

0.50

Item

c. Motor Bottle Cylindrical Outer Surface. ( 1 ) Scratches. Any scratch that penetrates the pro· tective finish into the metal is cause for rejection. If only the protective finish has been damaged, it may be repaired. ( 2) Dents. Any dent is cause for rejection. d. Missile Components. For maximum acceptable limits of damage to the surfaces of missile components, refer to DS maintenance. e. Air Vanes (flat Surfaces). ( 1) Depth of scratch or gouge: 0.02 inch ( 2) Width of scratch or gouge: 0.05 inch ( 3) Spa nwise (direction from inside edge to outside edge of vane) length of scratch or gouge: 3.0 inches ( 4) Chordwise (direction from leading edge to trail· ing edge of vane) length of scratch or gouge: 5.0 inches f. Air Vanes (Leading Edge). ( 1) Tip damage along leading, inner, or outer edges: 1.0 inch

I

(2) Total tip damage: 0.5 square inch ( 3) Depth of nicks: 0.1 O inch ( 4) Does not include more than three nicks (depths): 0.03 inch

I

g. Jet Vanes. Any damage to jet vane may be cause for rejection. Replace damaged jet vane and refer jet vane to OS for dye penetrant test and disposition.

C4

2-5

°'

N

1

SECOND STAGE

GUIDANCE SECTION

(>

(:

{

{

Figure 2-1. PERSHING missile.

NOTES: 1. AIR VANE 1 IS LOCATED UNDER HORIZONTAL MISSILE WHEN ON EL. 2. APPROX WEIGHT: 10,275 LB (4,664 KG).

AIR VANE LOCATIONS) (SEE NOTE 1

2

01Ii~

40.0IN.

(1.02 M)

FIRST STAGE

(

/ {

FSNB-5

WARHEAD SECTION

_)

\

r

CONTAINERS 2-2. Tabulated Data. Weights of tactically loaded truck M55 with: First stage in container ............... 32, 793 lb {14,874 kg) Second stage and guidance section in containers .......................... 33,480 lb {l 5, 186 kg) Warhead section in container ...... 27, l 06 lb ( 12,295 kg)

·..,.;

2-3. Humidity Indications. a. General. Table 2.3 lists the humidity indications for checking the internal relative humidity of missile section containers. For additional information related to humidity indi-1 cator, refer to TM 9-8140-380-24. b. Indicator Dot Color. ( 1 ) B (blue). Indicates that percentage of relative humidity is below number on dot. Example: If 30% dot is blue, relative humidity is below 30%. ( 2) L (lavender or white). Indicates that percentage of relative humidity is equal to number on dot. Example: If 30% dot is lavender or white, relative humidity is 30%. ( 3) P (pink). Indicates that percentage of relative humidity is above number on dot. Example: If 30% dot is pink, relative humidity is above 30%. c. Percentage of Relative Humidity. The relative humidity readings are accurate only if the container has been sealed for the previous 24-hour period.

C4

2-7

~

0

Co

N

1

p p

B B B B L

40

B B B B B L p

50 Desiccant control

Very good Good Poor Bad Bad Bad Bad

Percentage of relative humidity

Under 20 20 30 35 40 50 Over 50

Inspect every 24 hours. Inspect every 24 hours. Change desiccant. Change desiccant. Change desiccant. Change desiccant. Change desiccant.

Maintenance required 1

{'

(

(

{

(

(I

When missile section is in container, refer to TM 9-1410-375-12 for missile section and missile section humidity indicators maintenance.

p p p p

B B L

B L

p p p p p

30

Indicator dot color

20

Table 2-3. Relative Humidity Indications

/

I

I

\

N ID

n ...,

-

-

l_

BEARING SURFACE a9 . 0IN.(l.OO M)X 3.62 !N.(0.09 M) (TYP, BOTH SIDES) NOTE: EMPTY WEIGHT:

E

8 , 950 (4, 059. 72) 8, 950 (4, 059. 72 ) 8,950 (4, 059. 7 2) 8,950 (4, 059. 72)

e

F

E

DIM. 35.5 (0.90) 66.8 (1. 70) 35. 2 37.0 36.9 (0.89) (0. 94) (0.94) iO. l 63.3 64. 8 (1. 78) (1.61) (1.65)

37.4

37. 0

II. ... .,

BEARING SURFACE 57.0lN. (l,45M)X 3.62 IN. (0.09 M) (TYP, BOTH SIDES)

CONTAIN ER WITH STEEL COVE RS AND RINGS 3 , 710 LB (1,683 KG~ CONTAINE R W ITH ALUMINUM COVERS AND RIN GS 3 ,367 LB (l,527 KG).

.__t

3 . 75 JN.

I (0.10 M)

0

FSNB-17BI

62.9 64.1 63.3 64.8 (1. 60) (1.63) ( 1. 6 1) (1. 65)

Figure 2-2. First stage shipping and storage conta iner.

I

LIFT POINTS (TYP, BOTH SIDES)

36. 9

(J. 01) (0. 95) (0.94) (0.94)

39. 9

• • • • • • • •

C/ G LOCATION IN INCHES (METERS) TAC TNR !NERT MSL MSL MSL

EMPTY

(

QONTA!NER WITH STEEL COVERS AND RINGS •CONTAINER WITH ALUMINUM COVERS AND RINGS 144. 5 JN. - - -- - - (3.67 M ) - - - - - - l r 6 5 . 2 IN.

19,500 10,300 (8, 845. 20) (4, 672. 08) 10,300 19, 500 (8, 845. 20) (4, 672. 08) 19,500 10, 300 (8, 845. 20) (4,672. 08) 19,500 10,300 (8, 845. 20) (4, 672. 08)

-

TIEOOWN POINTS (TYP , BOTH SIDES)

D

c

B

A

MAX TIEDOWN LOADS IN POUNDS O
(

...

~

n

0

r~

(

-

OUTBD

(

II

e

F

E

DIM

•

..

35.7 (0.91) 70.2 (1. 78)

EMPTY

34.6 (0.88) 66.'7 (1.69)

-

•

39.9 (1. 01) 62.9 (1.60)

30.9 (0.78) 42. 5 (l. 08)

A 31.7 (0.81) 43.7 (1.11)

TNR MSL

.. •

37.4 (0.95) 64.1 (1.63)

TAC MSL

'""i

{

(

(,'

Figure 2-3. Second stage shipping and storage container.

~ Cl

1'«11 llRRPc

E

8,950 (4, 059.72) 8,950 (4,059. 72) 8,950 (4, 059. 72) 8,950 (4,059.72)

DOWN

•

36.9 (0.94) 63.3 (1.61)

.

{,

FSNB-16BI

64.8 (l.65)

37.4 (0.95)

INERT MSL

CONTAINER WITH STEEL COVERS AND RINGS A CONTAINER WITH ALUMINUM COVERS AND RINGS 144. 5 IN. i . . . - - - - - (3. 67 M)'-------<111>1 LIFT POINTS (TYP, BOTH SIDES)

-

BEARING SURFACE l_~• 39. 0 IN. (1. 00 M) X 3. 62 IN. (0. 09 M) (TYP, BOTH SIDES) NOTE: EMP.TY WEIGHT:

TOW POINT (TYP, BOTH SIDES)

TIEDOWN POINTS (TYP, BOTH SIDES)

D

c

~

-

A

AFT

10, 300 19, 500 (8,845.20) (4,672.08) 19,500 10, 300 (4,672. 08) (8,845. 20) 10,300 19,500 (8,845.20) (4,672 .08) 19,500 10, 300 (8, 845. 20) (4,672. 08)

FWD

POINT

C/0 LOCATION IN INCHES (METERS)

/

\

N

......

n ...,

(

-

B

LIFT

8,950 10,300 (4, 672. 08) (4,059.72) 8, 950 10,300 (4 , 672. 08) (4, 059. 72) 0

•

....

•

....

•

29.8 29.5 30.9 31.7 30. 9 0. 76) (0. 75) 0.78 ) (0.81) k0. 78) 43.4 45.3 42,5 43. 9 42.5 ( 1.10) (I.IS) (1.08) (I. 12) (1.08)

....

• ....

31. 7 31. 2 30.7 (0. 81) (0.79 0. 78) 43.7 45. 8 47.2 (l.ll) (1.16) (l.20)

INERT G&C

NO LIFT, NO T IEOOWN

I

4.0 IN. (0.10 M )

C ONTAINER WITH STEE L COVERS AND RINGS A CONTAINER W ITH ALUM INUM COVERS AND RINGS

e

c

D IM.

C/G LOCATION IN INCHES (METERS TNR EMPTY TAC G& C G&C

Figure 2 -4 . Guidance section shipping and storage co ntainer .

TOW POINT BEARING SURFACE - - - t..+--- 1---36. 0 IN. (TYP, BOTH SIDES) 22. 5 IN. (0. 57 M) (0.91 M) X 3. 62 IN. (0. 009 M) 89. 3 !N. I 65.0IN, (TYP,4 PLACES) (2. 27 M ) - - - - , ~(I. 65 M) NOTE : CONTAINER WITH STEEL COVERS AND RINGS 1,962 LB (890 KG ). EMPTY WEIGHT: CONTAINER WITH ALUM INUM COVERS AND RINGS 1,850 LB (839 KG). FSNB-IBBI

TOW POINT (TYP, BOTH S lDES )

TIEOOWN POINTS (TY P,BOTH SIDES)

(8,84~ . 2)

-

19,500 (8 ,845.2)

A

19,500

MAX TIEDOWN LOADS IN POUNDS (KILOGRAMS) DOWN POINT FWD A FT OUTBD

(

N

...~

FORK LIFT (TYP, EACH SIDE)

{

{.

_

{

{

.

{'

{1

FSNB-8

1. 50 IN. (0. 03 M) GRDCL AND SKID HEIGHT

'

ts;A;/~_l

--~--~--.

Figure 2-5. Warhead section shipping and storage container.

NOTE: EMPTY WEIGHT: 2, 316 LB (1, 050 KG).

TOW POINTS ( 2 EACH END)

~4,26M/

~--------':....__l67.90IN.

(2.11 M)

..__ _ _ 83. 0 IN •._ _ ___

/

\

r BLANKETS 2-4. Use of Blankets. - I._/

a. General. All missile sections can be stored in containers at temperatures as low as -31.7°C (-25°F) without use of heating blankets. b. First and Second Stage Blankets. First and second stages in containers can be exposed to temperatures as low as -53.8°C (-65°F), with wind velocities up to 40 mph (64 kmph), for up to 1 week after removal of power for heating or after a temperature drop, providing the sections have previously been conditioned to -6.7°C (20°F). Hydraulic actuator blankets are used during the confidence and standard countdown when the ambient ternperature is -6.7°C (20°F) or below and 30 minutes prior to starting the power station when the ambient temperature is -31.7°C (-25°F) or below. Refer to TM 9-1410-375-12 for procedures for installing and removing first stage and second stage blankets.

I

c. Guidance Section. If a missile is to be fired in a minimum time period, the guidance section must be preconditioned. Refer to TM 9-1410-375-12 for procedures for preconditioning the guidance section. d. Warhead Section. The warhead section conditioning kit must be installed when the ambient temperature is -31.7°C (-25°F) or lower. If the missile is to be fired in a minimum time period, the warhead section must be preconditioned to operating temperature. Refer to TM 9-1425-381-10 for procedures for preconditioning the warhead section, and installing and removing the warhead section blanket.

C4

2·13

I

r

•'t

.

~

\

0\,_·_ ''" ~\ "'

2-14

...

U'I

....~

(

{

1 2 3 4 5 6 7 8 9 10 11 12

-

{1

Legend.

Initiator access flap Hoist point access flap (2) Lanyard Main blanket section Hydraulic actuation package access flap (2) Power connector Hoist point access flap (2) Tail plug access flap End cover (2) Zipper Closing strip Lanyard

Figure 2-6. First stage blanket -

(

(

(

~

~

2-16

........~

(

{

(

-

{

Legend.

Lanyard Small blanket closing strip Top band Interconnecting power cable Hoist point access flap (2) Initiator access flap (2) Connecting strap Front blanket section Bottom band Lanyard Rear blanket section Hydraulic actuation package access flap (2) Power connector Hoist point access flap (2) Overlap flap End cover (2) Zipper Closing strip Connecting strap

Figure 2-7. Second stage blanket -

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19

{

(

~

~

r

2

6

4 5

FSNB-25

1 2 3 4 5 6 7

-

Main blanket Cable mast hood Power connector Front end cover Rear end cover Umbilical door access flap - Porro prism access flap

Figure 2-8. Guidance section blanket.

2-18

IO

I\)

...

REAR FLAP

HEATING BLANKET

HOOK TAPE

ST RAP (2) LE NGTH 36 FT

Figure 2-9. Warhead section blanket.

ST RAP (3)

I

PILE TAPE

ELECT RICAL CONNECTOR (2)

(.

(

FSNB-29

END COVER

(_

HOISTING BEAMS

2-5. Ancillary Equipment Tiedown Kit. The tiedown ki t consists of webbing straps a nd r etaining and mounting brackets that sec ure the support tu bes and disassem bled hoisting beams to wrecker M543. Stor e the fo llowing as shown in figure 2- 11: frames ( forward and rea r ) and spreader and chann el bea ms of the fir st and second stage hoisti ng beams; suppo rt t ubes; and sections (forward and r ea r ) and t ube assembly of the gu idance section hoistin g bea m.

2-20

51.42 IN. I~ -47.18 IN. (1.31 M)"'t ~ (1.20 M)

B. FOR FIRST OR SECOND ST AGE

NOTES: 1. GUIDANCE SECTION HOISTING BEAM WEIGHT: 51 LB (23 KG). 2. FIRST OR SECOND STAGE HOISTING BEAM WEIGHT:246 LB (111 KG).

FSNB-4

Figure 2-10. Hoisting beams.

2-21

FSNB-26

1 2 3 4 5 6 7 8

...: -

9 1O 11 12 13 14 15 16 -

Strap assembly Support tube (4) and spreader beam assembly (2) Strap assembly Strap assembly Retaining bracket Channel beam (right a nd left) (4 ) Retaining bracket Frame (forward and rear), section (forward and rear), and tube assembly Strap assembly Storage bracket Strap assembly Strap assembly Strap assembly Frame (forward a nd rear) Strap assembly (3) Mounting bracket (2)

Figure 2-11. Hoisting beam storage on wrecker M543.

2-22

r

CHAPTER 3 ERECTOR-LAUNCHER (CONTENTS) Item

EL electrical circuit test set .............. . EL electrical circuit test set indicator functions ..•.•..•.•.•.•.•.••.••......•••.••.••. 'W EL (less missile) physical data •.•...••.• EL (with missile and XM757) transportation data •.•.•..•.........•.••.. Functional data •..•...•.•.•.•...•.•••••....••.. Physical data .•...•.•..•..•.•.•....••.•.•.•.•••. Warhead section handling device..•..•.

Reference Par. 3.3 Table 3-1 Fig. 3·1 Fig. Par. Par. Fig.

3-2 3-2

Page

3-8 3-8

3-6· 3-5

3-3

3-1

3-3

3-3

3-7

""""

3-1

r

r CHAPTER 3 ERECTOR-LAUNCHER ~

3 -1 • Physical Data • a. Weight. EL with cable mast ........................... 18,727 lb (8,495 kg) Cable mast .............................................. 308 lb ( 140 kg) EL .................................................. 18,497 lb {8,390 kg) I Azimuth ringassembly .......................... 1,433 lb (650 kg)· Front jack ............................................... 290 lb ( 132 kg) Rear jack ................................................ 312 lb ( 142 kg) Hydraulic oil tank ..................................... 95.6 lb ( 43 kg) b. Wheels. Size ........................................................ 19.5 by 13.0 in. c. Pneumatic Tires. Size ............... 16.5 by 19.5 in. 10 ply (plus 1 breaker ply) Rating .......................................................... 16 ply rating Operating pressure (nominal) ........................... 45 psig air d. Hydraulic Reservoir Capacity. Full (upper line on sight gage) ........... 33 gal ( 124.9 liters) (Use hydraulic oil MIL-H-81019 (FSN 9150-935-7148) or MIL-H-5606 (FSN 9150-265-9408).) e. Fire Extinguishers. Type .......................................................Vaporizing liquid Extinguishing agent ................. Monobromotrifl uorom ethane Stabilizing agent .................................................. Nitrogen

f. Davit Assembly. Lifting capacity ..................................... 1,300 lb ( 590 kg)

'-" 3-2. Functional Data. a. EL Input Requirements. Electrical. ................... 120/208v, 3-phase, 400-Hz, 45-kw generator. (Use 10-kw generator for limited use) Pneumatic: Cable mast assembly and clamp release mechanism ............................... 3,000 psig air Hydrau1ic accumulator (precharge) ........... 850 to 1,000 psig nitrogen (925 to 1,000 psig when operating in temperature below -31.7°C (-25°F)) b. EL and Tractor XM757 Turn Radius. Left turn ....................................................42.5 ft ( 13 m) Right turn ..................................................42.5 ft { 13 m)

C3

3.3

I

r

\

I

c. Travel and Emplacement Limits. Maximum tractor XM757 and EL cruising speed (improved roadway) ................ 50 mph (81 kmph) Maximum ground slope for EL emplacement. .................. 6° Maximum wind velocity (with missile erected) ................... 40 mph (64 kmph) steady; 60 mph l. 1 (97 kmph) gusts.._., Maximum fording depth ............................ 40 in. ( 102 cm) d. Change of Azimuth Method and Limits. Method ............................................ Manual (crank) drive Limits ............................. 1,582 mils to either side of 0 mil

3.4

C3

UI

't'

n ._.,

(

(

{

( (

NOTE:

Figure 3-1. EL (less missile) physical data.

WEIGHT: 18,727 LB (8,495 KG).

j_

(2. 75 M)

REDUCIBLE TO 108.45 IN.

(2.97 M)

T 117.tIN.

FSNB-22BI

TIEDOWN LIMIT LOADS IN POUNDS UCILOGRAMS> POINTS ( TYP BOTH SIDES ) :FWD AFT INBD OUTBD UP DOWN a 15, 000 (6, 804) 15. 000 (6, 804) 15, 000 (6. 804) 15. 000 (6, 804) 30. 000(13, 608 30. 000(13, 608) b,h 36. 000(16, 330) 36, 000(16. 330) 9, 4110 (4, Z87) 9,450 (4,4'1111 ~6. 000(16,330) 6. 000(16,330) c,d 22. 500(10, 206) 22. 500(10, 206) 22. 500(10. 206) 22. 500(10, 206) 45, 000(20, 412) 5. 000(20. 412) 45. 000(20, 41.r; 115. 000(20, 412) 30. 000(13, 608) 30. 000(13, 608) 30. 000(13, 608) 0, 000(13. 608) e,f g 45, 000(20, 412 45, 000(20, 412) 15. 000(6, 804) 15, 000 (6, 804) 45,000(20,412) 5,000(20, 412)

(

_)

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fl

0.

w

a

450.75 IN.( 11.45 M)

(

('

(

•I

I

AZIMUTH MANUAL DRIVE (REMOVABLE)

{

(

(

NOTES: 1. TURNING RADIUS: 42.5 FT (12.95 M). 2. AXLE LOADS: A & B-10,336 LB (4,688 KG) EACH. C & D 4 6,397 LB (2,890 KG) EACH. E & F-6,306 LB (2,860 KG) EACH. 3. WEIGHT: 46,546 LB (21,113 KG). • FSNB-2IBI

Figure 3-2. EL (with missile and XM757) transportation data.

1 1 9 - - - - - - - - - - - 5 7 0 . 0 IN. (14.48 M)

g i,j,k,1 m,n

e,r

c,

b,h

)

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.:...

w

w

(")

(

HOLE A (WS +SLING) AND SHACKLE HOLEC (DO NOT USE)

HOLED (WS + SLING + CRADLE) HOLE B (SLING ONLY OR SLING + CRADLE)

16.4 IN. (0.42 M)

{

:I

-========!================-_.l___t

(

Figure 3-3. Warhead section handling device.

FSNB-20CI

-===="~-!JM).

{

~ . .L

(

57.8 IN, (1.47 M) - - - - - - - - - - 148.5 IN. j.-40.5 IN. NOTES: (3. 77 Ml (1,03 M) l. EMPTY WEIGHT: SLING -228 LB (103.4 KG) CRADLE -267 LB (121. l KG) SLING + CRADLE -495 LB (224.S KG) 2. USE HANDLES ON FORWARD COVER ONLY FOR GUIDING PROTECTOR-SLING. 3. ATTACH BELT TO SLING BEFORE MATING WS TO SLING.

{

~

3-3. EL Electrical Circuit Test Set. a. The EL electrical circuit test set {tester), with decables 98W 1, 98W2, and 98W3 is used to locate and isolate electrical malfunctions in the EL or to verify the operation of the EL. b. Table 3-1 lists the functions of the indicators on the...._., tester. An indicator lights when an electrical command or voltage reference of the EL under test is being verified.

1 tachable

~

Table 3-1. EL Electrical Circuit Test Set Indicator Functions Indicator

Function

AlJ2 5 6 10 11 15 16 18 19 22 23 24 27 28 30 31 32 33 35 37 40

Dangerous tilt (PTS) Warhead mated EL charging EL charged EL leveling ST-120 platform heater EL level Erect No. 1 supv Auto seq selected MSL vertical Boom clear Spare Spare Spare LlO bus ac Spare Spare Spare Horn voltage MSL thermostat

"-r"

AlJ4 1 2 3 4 5 6 7

3·8

Shut off valve supv Front manual sw retract Curb manual sw retract Road manual sw retract 28vdc supply supv Uplocks Front manual sw extend

C2

r

~ Table 3-1 • EL Electrical Circuit Test Set Indicator Functions-Continued

....

Indicator

Function A1J4-Continued

-'

8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 thru 41 42 43 44 45

Curb manual sw extend Road manual sw extend Pump enable Final pressure S4 Boom down supervision Spare Pump motor ST-120 temp ok Rear low Front low Curb low Road low Front jack temp supv Final pressure Dangerous tilt slave Boom down Auto level Launch pad up supv Solenoid down supv Front jack retract Solenoid up supv Front jack extend Curb jack extend Curb jack retract Road jack extend Road jack retract Curb jack temp supv Dangerous tilt (output) Boom clear Standby Spare Level condition Road jack temp supv Spare + 28v ( + 0400) bus supv

3.9

r

Table 3-1. EL Electrical Circuit Test Set Indicator Functions-Continued Indicator

Function AlJ4-Continued

46

Spare

thru

50 51 52 53 54 55 57 58 59 60

3-10

Pump voltage-ac Curb j ack motor - ac Front jack motor-ac Road jack motor-ac LlO to de supply-ac L20 to de supply-ac L30 to de supply-ac Spare Spare

-,

r CHAPTER 4 PROGRAMMER-TEST STATION (CONTENTS) Item Adapter diagnostic test modes ......... . Adapter malfunction display codes ... . CMTS malfunction display codes ...•... Conditions causing short hold that operator can control. ..........•..•....... Conditions causing short hold that operator cannot control ................ . Jumper cap information •.................. Manual data entry •....•........•..•.........• Power distribution buses ......•........... Program tapes and containers ......... . PTS interior, left side .........•............. PTS interior, right side .................... . PTS shelter physical data ................ . PTS·PS transportation data ............. .. Quick count sequence ......................... .

Signals on connector pins of PTS cable entry panels ....................... . Standard count sequences ................... .

C4

Reference

Page

Par. 4.5 4-32 Table 4.4 4-12.51 Table 4.5 4·14.1 Table 4-2

4-9 ~

Table 4-3 Table 4·8 Par. 4-1 Table 4.7 Table 4·1 Fig. 4.3 Fig. 4-4 Fig. 4·1 Fig. 4-2 Par. 4-3

4-12 4.33 4.3 4-31 4-9 4.37 4-38 4-35· 4-36 4·7

Table 4-6 Par. 4-2

44~~,

4·1 /(4·2 blank)

1

I

r

CHAPTER 4 PROGRAMMER-TEST STATION I._,) 4-1 • Manual Data Entry.

a. 01 SPL (Spheroid of Launch). Represents firing PO· sition location in one of six spheroids of the earth. This value is used to compensate for curvature of earth in the specific spheroid. 0 International 1 Clarke 1866 2 Everest

3 Clarke 1880 4 Bessel 5 Clarke 1858

b. 02 AOL (Altitude of Launch). Represents altitude in meters of firing position above ( +) or below ( - ) sea level. c. 03 ZOL (Zone of Launch). Firing position in one of 60 zones of earth in the UTM system. Zero is used for this entry when Geographic system is used. Note In determining EOL (d below) and the EOT (k below), it should be noted that the westmost position of zone is 150,000 meters, midzone is 500,000 meters, and eastmost position of zone is 850,000 meters. Therefore, EOL and EOT must be somewhere between 150,000 and 850,000 meters.

-.,,,,,,;

d. 04 EOL (Easting of Launch). UTM system. Firing position in meters as measured on an east-west line in zone which the missile is located. e. 04 LAL (latitude of Launch). Geographic system. Firing position in Northern ( +) or Southern ( - ) Hemi· sphere. Value is in degrees, minutes, seconds and tenths of seconds. Never greater than 90 degrees. f. 05 NOL (Northing of Launch). UTM system. Number of meters north or south of equator. Northern Hemisphere 0 to · 10,000,000 meters from equator to north pole. Southern Hemisphere -10,000,000 to -0 meters from equator to south pole. g. 05 LOL (Longitude of Launch). Geographic system. Represents firing position in Eastern ( - ) or Western ( +) Hemisphere. Value is in degrees, minutes, seconds, and tenths of seconds.

4.3

h. 06 SPT (Spheroid of Target). Same as SPL, except that it represents location of target.

i. 07 AOT (Altitude of Target). Same as AOL, except that it represents altitude of target.

I

j. 08 ZOT (Zone of Target). Same as ZOL, except that it rep· resents zone of target.

k. 09 EQT (Easting of Target). Same as EOL, except that it represents location of target.

I. 09 LAT (Latitude of Target) . Same as LAL , except that it represents location of target. m. 10 NOT (Northing of Target) . Same as NOL, except that it represents loca tion of target. n. 10 LOT (Longitude of Target). Same as LOL , except that it represents loca tion of target. o. 11 HOB ( Height of Burst) . First digit represe nts type of burst. Air burst 2 Air I surface burst 3 Surface burst The r emainder of th is entry specifies height in meters above target at which warhead detonation will occur. p. 12 TAT (Target Atmosphere). A numeric va lu e of one or two digits representing atmosphere of target. Th e TAT selected mu st co rrespond to one of three TATS selec ted at start of count.

I 4-2.

Standard Count Sequences.

a. Program Entry. ( 1) System cabl es connected. (2) Firing position equipment readied for countdown. (3) Block I of countdown tape loaded. (4) Checksum of memory. (5) TATS se lected. ( 6) Block 11 of countdown tape loaded and tape is rewound . b. Computer Self·Test. ( 1) Che ck of te leprinter. (2) Checksum of memory. (3) Mode selection (confidence, standard , quick).

4 -4

C4

r

( 4) Computer self-test. c. Manual Data Entry. ( 1) Enter set number. (2) Enter MDE's.

~

(3) Compute firing equations. d. Adapter Self·Test. ( 1) Perform limited self-test of adapter. (2) Display FAM.

"..I

e. Initial Monitor. ( 1) Cable checks. (2) Missile identification check. f. Monitor Scan. Start monitor scan. (Repeated at I-second intervals throughout program.) g. Missile Power. Power applied to missile. h. Range Select. ( 1) Range selection applied to missile. (2) Voltage check of missile buses. (3) Inverter voltage monitor. i. Set T and Offset Integrate. ( 1) Set T test. (2) Offset velocity integrate test. j. Warhead Preset and Verification. Warhead preset and ver· ified for flight. k. Guidance Computer Test. "(1) Preset integration test.

(2) Inverter voltage and frequency monitors. I. Platform Enable. Uncage ST-120. m. Set ERB·Fast Erect. Ball and disc integrate. n. Set ERB-Slow Erect. o. SA+CR Arm Test. ( 1) Platform level test. (2) Pitch program test. p. Controls Test. (1) Gimbal temperature check.

\._,}

(2) First and second stage pumps on.

C4

4.5

(3) Control seal-in test. (4) Test of control computer and actuators. q. Simulated Flight. Simulated flight test. r. Azimuth Lay Coarse. ST ·120 torqued to firing azimuth. s. Guidance Preset and Verification. ( 1) Preset SRV and SRO. (2) Verify SRV and SRO. t. Azimuth Lay Fine. u. Acceleration Monitor. (1) · SR accelerometer.

(2) CR accelerometer. (3) SA accelerometer. v. Burst Select. ( 1) Air, surface, or air/surface select. (2) Lay complete.

w. Preremote Monitor. (1) EL charged and level. (2) Select auto sequence. (3) Azimuth ring clamp removed monitor. (4) Arm launch control panel. (5) Select remote. x. Remote. (1) Clear area warning. (2) Inverter frequency and voltage monitor. y. Launch sequence initiation. ( 1) Fire switches pressed. (2) 3,000 psi monitor. z. Erection. ( 1) First and second stage pumps on. (2) Missile vertical supervision. (3) Battery activate. aa. Fire Sequence. ( 1) EBW monitor. (2) Control seal·in monitors. (3) Vane lock.

4-6

C4

r (4) Battery voltage check. (5) Fire explosive switches. (6) Mast eject. (7) First stage ignition.

- \_,I

(8) Lift-off.

I

4-3. Quick Count Sequence. a. Program Entry. Terminate alert readiness. b. Computer Self-Test (not performed in quick count). ( 1) Check of teleprinter. (2) Checksum of memory. (3) Mode selection.

~

c. Manual Data Entry. Enter set number. d. Adapter Self· Test. Perform limited self-test of adapter (CMT, CRG, MMO, PON). e. Initial Monitor. ( 1) Cable checks. (2) Missile identification check. f. Monitor Scan. Start monitor scan. (Repeated at l·second intervals throughout program.) g. Missile Power. Power applied to missile. h. Range Select. ( 1) Range selection applied to missile. (2) Display FAM.

(3) (4)

Inverter voltage monitor. Verify SRV preset.

i. Platform Enable. Un cage ST -120. >.._)

j. Set ERB-Fast Erect ( 1) ERB prep. (2) Gimbal temperature check. k. Burst Select. ( 1) Burst selection verified.

~

(2) Set ERB.

I. Auto Slew.

C4

4.7

m. Azimuth Lay Coarse. ST·l20 torqued to firi ng azimuth. n. Acceleration Monitor. ( 1) SR accelerometer. (2) Lay complete. o. Prerem ote Monitor. ( 1) EL charged and level. (2) Azimuth ring switch supervisio n. ( 3) Arm laun ch control panel. ( 4) Select remot e. p. Remote. ( 1) Clear area warning. (2) Inver ter voltage and frequency monitor. q. Launch Sequence Initiation. ( 1) Fire switches pressed. ( 2) 3000 psi monitor. r. Erection. (1) Fi rst and second stage pumps on.

(2) Missile vert ical supe rvi sion. ( 3) Battery activate. s. Fire Sequenc e. (1) EBW mon it or.

(2) Control seal·in monitors. (3 ) Vane lock.

(4)

Battery voltage check.

( 5 ) Fire explosive switches.

(6) Ma st eject. (7) First stage ignit ion. (8) Lift -off .

4-8

C4

r Table 4-2. Conditions Causing Short Hold That Operator Can Control-Continued Phase/IRI display Missile Power TURN MSL ON L-J

...,.

Condition

Missile power not turned on.

Set T None

C3

4-8.1/(4-8.2 blank)

·~\

'I

.-

~

r Table 4-1. Program Tapes and Containers Container/tape reference No.

Item

",../

11051854/11051804 11051851/11051801 11051860/11052764

Adapter diagnostic CMTS diagnostic Computer diagnostic \._/

·~

Individual missile sections in-container

11051852/11051802

Missile less warhead section in-container

11051853/11051803

Tactical program tape

11051862/11051812 11051855/11051805

Tactical training program tape

11051865/11051815 11053110/11053060

UUT tapes for CMTS

I

I

Table 4-2. Conditions Causing Short Hold That Operator Can Control Phase/IRI display ~

Condition

Ground Power and TAT Selection None MOE, Self-Test, and Initial Monitor PRINT INOP

Printer not turned on or not op· erating. (Refer to paragraph

3-27.) KEY SW TO LOCAL

MTEWH 1

LOCAL/REMOTE key switch turned to REMOTE. Turn switch to LOCAL and press COUNTING switch. EL control panel warhead switch not set to WHO MATED.

See footnote at end of table. C4

4-9

r

I

'\

Table 4-2. Conditions Causing Short Hold That Operator Can Control-Continued Phase/IRI display EL PREP'

ACT CLD 1

-

Condition

EL control panel MODE selector switch not turned to LOCAL and/or automatic leveling not initiated. Oil temperature of hydraulic actuation assemblies below -31.7°C (-25°F). Notify supervisor of display. When directed by supervisor, press COUNTING switch. SAFE/ ARM switch not turned to SAFE. ~ EL control panel MODE selector switch turned to AUTOMATIC SEQUENCE. Request supervisor to direct EL operator to turn MODE selector switch to LOCAL. Azimuth ring clamp sections not installed.

'-"

SAFE LCP IMP EL MODE

MTE CLMP 1 Missile Power TURN MSL ON

Missile power not turned on.

SetT None Warhead Preset and Verification None Guidance Computer Test None Controls Test None Simulated Flight None Guidance Preset and Verification LAY TMR

MONITOR switch not pressed.

'91

See footnote at end of table.

4-10

C4

r

Table 4-2. Conditions Causing· Short Hold That Operator Can Cont'•~Continued Phase/IRI display

Condition

-~

Accelerometer Monitor AIR SUR A/S ~

Horizontal Laying Verification IMP EL MODE

MTE CLMP 2 CNF CD 4

EL control panel MODE selector switch turned to AUTOMATIC SEQUENCE. Request supervisor to direct EL operator to turn MODE selector switch to LOCAL. COMPLETE (or LAY COMPLETE) switch not pressed. Missile erection for vertical lay. SAFE/ARM switch not turned to SAFE. EL control panel MODE selector switch not turned to AUTO· MATIC SEQUENCE. SAFE/ARM switch not turned to ARM. Azimuth ring clamp sections in· stalled. Theodolite operator requires more time to lay the ST-120. MONITOR switch not pressed. Prepare for vertical lay remote phase or for standard (or quick) erect and fire. Prepare for vertical lay erection. End of confidence count.

Remote RMTE RECYCL 3

Selected recycle to laying phase.

'.,I

LAY COMPL VL 2 SAFE LCP 2 AUTO SEQ 3 ARM LCP 3 REM CLMP 3 LAY RECYCL LAYTMR SEL RMTE3

1...,1

1

2 3 4

'.I

MDE specified air burst. MDE specified surface burst. MDE specified air burst with sur· face backup.

Hold not applicable for a quick erect and fire sequence. Hold applicable only for vertical laying. Hold not applicable for a confidence count. Hold applicable only for a confidence count.

C4

4.11

i

Table 4-3. Conditions Causing Short Hold That Operator Cannot Control Phase/IRI display

Condition

Ground Power and TAT Selection None

'\

Remarks Note The time intervals specified below assume usual environmental conditions and no operator errors. If specitied hold time intervals are exceeded, notify supervisor before proceeding with maintenance.

MOE, Self-Test, and Initial Monitor

~

~

'-1'

None Missile Power NO 1200 PSI

High-pressure air pressure below 1,200 psig.

2 minutes

PLT CLO

ST-120 base plate temperature below 0°C (32°F).

1 minute

GD CMP CLO

Guidance computer ternperature below 6°C (42.8°F).

1 minute

Set T None Warhead Preset and Verification None

---

...... 4-12

C4

r Table 4-3. Conditions Causing Short Hold That Operator Cannot Control-Continued Phase/IRI display

Condition

- ....,_J

Remarks

"I

Guidance Computer Test INVR FRQ 1

Missile inverter frequency not stabilized.·

After approximately 4 minutes sequence will mal· function with CD MALF TEST 187 G+C INVR dis· played on IRI.

PLT PREP

ST-120 power on and stabilizing sequence.

After 2 minutes, sequence will auto· matically advance.

GMBL CLD 2

Gimbal ternperature below 32°C (89.6°F).

2 minutes Note GMBL CLO may be displayed for as long as 10 minutes if the fire sequence was terminated for as long as 30 minutes and the guidance section was allowed to cool during this time.

GMBLHOF

Gimbal tern· perature above 45°C (113°F) or gimbal air ternperature above 10°c (158°F).

5 minutes

PLT LEV

ST-120 leveling.

20 minutes

'..._)

See footnote at end of table. \.._)

C4

4-12.1

f

'\

I

Table 4·3. Conditions Causing Short Hold That Operator Cannot Control-Continued Phase/IRI display

Condition

Remarks ~

Controls Test GMBL CLD 1


2 minutes Note GMBL CLD may be ~ displayed for as long as 10 minutes if the fire sequence was terminated for as long as 30 minutes and the guidance section was allowed to cool during this time.

"-"

GMBL HOP

Gimbal ternperature above 45°C (113°F) or gimbal air ternperature above 70°C (158°F).

5 minutes

GMBL CLO


2 minutes

GMBL HOT

Gimbal ternperature above 45°C ( 113°F) or gimbal air ternperature above 70°C ( 158°F).

5 minutes

Simulated Flight None Guidance Preset and Verification ~

~


4-12.2

~

C4

r

~

I

Table 4·3. Conditions Causing Short Hold That Operator Cannot Control-Continued , Phase/IRI display

Condition

Remarks

-~

Accelerometer Monit or SA CAM 1

Slant altitude program cam not at zero.

NO 2300 PSI

High-pressure air 2 minutes pressure in guidance section gyro air sphere below 2,300 psig.

~

~

After approximately 4 minutes, sequence will malfunction with CD MALF TEST 370 ADPT or CD MALF TEST 371 G+C GD CMP displayed on IRI.

Horizontal Laying Verification NO 2300 PSI

2 minutes High-pressure air pressure in guidance section gyro air sphere below 2,300 psig.

BATTMP

Missile batteries temperature too low.

10 minutes

EL CHG

EL accumulator not fully charged.

1 minute for -31.7°C (-25°F) and above; 10 minutes for below -31.7°C

EL LEV

EL leveling.

1 minute

BRG AIR HTR

ST-120 fro bearing air eaters have not cycled.

2 minutes

\,../


C4

4-12.3

Table 4·3. Conditions Causing Short Hold That Operator Cannot Control-Continued Phase/IRI display GMBL HOT

Condition Gimbal ternperature above 45°C (l 13°F) or gimbal air temperature above

Remarks 5 minutes

70°C (158°F). Vertical Laying and Verification GMBL CLO

Gimbal ternperature below

2 minutes

32°C (89.6°F). GMBL HOT

Gimbal ternperature above 45°C (1 l3°F) or gimbal air temperature above

5 minutes

70°C (158°F). Remote None Firing None 1Hold 2 Hold

4·12.4

not applicable for a quick erect and fire sequence. applicable only for a quick erect and fire sequence.

C4

Table 4-4. Adapter Malfunction Display Codes

Area mnemonic code ADPT MALF 1

AFM ALG AZCB BAT ACT INT 1

Meaning Adapter malfunction Acceleration and frequency monitor Alinement amplifier Azimuth laying control box Battery activate interrupt

I See footnote at end of table.

C4

4-12.5/(4-12.6 blank)

r

r

Table 4-4. Adapter Malfunction Display Codes-Continued Area mnemonic code CMD PAR 1 CMP MALF 1 CMP TMR 1 CMT "'RB 1 '-'ERG

1..,1

Meaning Command parity error Computer malfunction Computer timer Constant monitor Crowbar Control register a. Command module b. Column selection c. Monitor zero d. Emitter follower and row selection e. Relay matrix

OTA PAR 1 0102 INT 1 0103 INT 1

Data parity error 0102 interrupt 0103 interrupt

FIRE 0 INT1

Fire zero interrupt

GNCJ

Interlock test, test cable entry, mode 02

HEFU HEFU INT 1

High energy firing unit High energy firing unit interrupt

LCP

Launch control panel

LPON

Limited power on

MALF TEST 000 MALF TEST 000 CKSUM MALF 1 \_J\llALF TEST 000 .._.. CMP TMR 1 MALF TEST 000 CROWBAR INT MALF 1 MALF TEST 000 L--1 CROWBAR .._,. MALF 1 MISC MMO MSL PWR OFF 1 .,ON ~ PRINT INOP

Power malfunction Checksum malfunction Computer timer Crowbar interrupt malfunction Crowbar circuit ( 32A2A7A85) malfunction Miscellaneous test Monitor module on Missile power off Remaining adapter power on and miscellaneous tests Printer inoperative


C3

4-13

r

Table 4-4. Adapter Malfunction Display Codes-Continued Area mnemonic code

Meaning

PVC PPS PRS

Programmable voltage comparator Programmable power supply Presetting circuits

RATIO MALF 1

Rf BX

PVC ratio malfunction Remote firing box

SFTY REL I NT 1

Safety relay interrupt

TCTB

TMR INT 1 TMER TRS 1

Interlock test, tactical cable entry, mode 00 Interlock test, tactical and fire control'-" cable entry, mode 01 Programmable timer interrupt Programmable timer Transient interrupt

WH CONT INT 1

Warhead continuity interrupt

1J02 1J03 1J04 1J05 1J06 1J07 !JOB 1J09 lJ 10

32A4A1J2, tactical cable entry 32A4AlJ3, tactical cable entry 32A4A1J4, tactical cable entry 32A4AlJ 5, tactical cable entry 32A4AlJ6, tactical cable entry 32A4A1J7, tactical cable entry 32A4A1J8, tactical cable entry 32A4A1J9, tactical cable entry 32A4A1J 10, tactical cable entry

1SGJ

Interlock test, test cable entry, mode 03i._.,

2J01 2J02 2J03 2J04 2J05 2J06 2J07 2J08

32A4A2Jl, 32A4A2J 2, 32A4A2J3, 32A4A2J4, 32A4A2J5, 32A4A2J6, 32A4A2J7, 32A4A2J8,

TCTJ

test cable test cable test cable test cable test cable test cable test cable test cable

entry entry entry entry entry entry entry entry

2SGJ

Interlock test, test cable entry, mode04

5J06

32A4A5J6, fire control cable

1

entry~

These area mnemonic codes are random displays that can be displayed at any time during the automatic adapter diagnostic test.

4-14

Cl

r

Table 4- 5. CMTS Malfunction Display Codes Area mnemonic code

Meaning

ADPT MALF ADAPT PPS A91

Relay write malfunction Adapter programmable power supply Module test connector

BATT ACT INT

Battery activate interrupt

CK SUM ERROR CMD PAR CMP MALF CMP TMR CRB CRG

Program not complete in memory

CTAC CT PPS OTA PAR

0102 INT 0103 INT

Command parity error Com put er ma If unction Computer timer malfunction Crowbar malfunction Control register a. Command module b. Column selection c. Monitor zero d. Emitter follower and row selection e. Relay matrix Card tester ac power CMTS programmable power supply Data parity error Bus +0102 interrupt Bus +0103 interrupt

ENTRY ERROR

Keyboard entry error

FIRE 0 INT

Fire zero interrupt

HEFU INT

High energy firing unit interrupt

J26 J27 J28 J29

Relay cards test connector Adapter cards test connector Alinement amplifier card testconnector Computer logic cards test connector Computer memory cards testconnector

J30 LIT MALF TEST 000 MALF TEST 000 CROWBAR INT MALF MALF TEST 000 CROWBAR MALF

C3

Load simulation Power ma If unction Crowbar interrupt Crowbar circuit malfunction

4-14.1

Table 4-5. CMTS Malfunction Display Codes-Continued Area mnemonic code

MDC MIST MMO MSL PWR OFF PON PPS

4-14.2

Meaning Module circuits Miscellaneous test Monitor module on Missile power off Remaining adapter power on and miscellaneous test Programmable power supply

C3

r

'

I

Table 4-5. CMTS Malfunction Display Codes-Continued Area mnemonic code

~

PPSA PUDE PUSE PVC

Meaning CMTS programmable power supply Pulse detector Pulse sequencer Programmable voltage comparator

RATIO MALF

Ratio measurement

SFTY REL INT

Safety relay interrupt

TAPE PARITY TEST NOT FOUND ~ TMR INT TPOA TRS TRMA WH CONT INT

C2

Tape reader parity error Programmable timer output interrupt Card tester power on Transient interrupt Ca rd tester relay matrix Warhead continuity interrupt

4-15

.c:i.

(')

...en~

{)

{1

(,

Air select command Air select supervision Air/surface select command Air/surface select supervision Attitude signal excitation off command Auto sequence selected Azimuth pickoff output Azimuth positioning signal Azimuth ring switch supervision Azimuth ring switch supply Battery activate command Battery activator and case venting safe supervision Battery activator arm command Battery heater supply (LlO) Battery heater supply (l20) Battery heater supply (l30) Battery heater supply (neutral) Battery temperature low supervision

Tactical Cable Entry Panel (A4Al)

Signal

J6-20 J6-18 J6-7 J6-29 J5-23 J 10-13 J8-43, 44 J2-28, 29 J9-53 J9-58 JS-6 JS-7 JS-5 JS-2 JS-3 JS-4 JS-1 JS-14

(

Connector pin(s)

I

{

(

El3 Bl3 012 M13 All l24 L20, M20 K2, J2 E24 A31 BlO ClO AlO N39 L39 M39 N28 HlO

Signal distribution box (32A8) test points

Table 4-6. Signals on Connector Pins of PTS Cable Entry Panels

/

\

I

I

.......~

n

(

(

( (

Signal

Bearing airflow reduction command Bearing air heater off command (minus) Bearing air heater on supervision Bearing air 1200 PSIG switch supervision Bearing air 1200 PSIG switch supervision supply Bearing air 3000 PSIG switch supervision Bearing air 3000 PSIG switch supervision supply Cage-uncage motor (LlO) Cage-uncage motor (l20, l30) Cage-uncage motor (neutral) Cage-uncage supervision supply Caged supervision Control computer on command Control seal-in off command Control seal-in on command Control seal-in on supervision CR integrator stop command

J9-19 J5-13 J5-24 JS-12 JS-13 JS-10 JS-11 JS-58 JS-60 JS-59 JS-20 JS-21 J4-47 J9-6 J4-32 J4-33 J3-49

Connector pin(s)

H7

MS A9

H34 013 811 019 F19 C19 J13 H19 L35 K35 F19 G19 H9 E22


Table 4-6. Signals on Connector Pins of PTS Cable Entry Panels-Continued

(

Tactical Cable Entry Panel (A4Al)-Continued

(

~

I

~

.J:lo

(")

00

...~

{)

{\

(

CRO hold command CRO monitor and substitute command CRV hold command CRV monitor and substitute command CRV monitor ( Sl, S2, S3) CRV offset command CRV zero command Cutoff test supervision Cutoff test supervision supply +010 +28v de monitor +02 + 25v de power supply - 02 - 25v de power supply +011 +28v de power supply +02 +25v de power supply Emergency missile power off command (negative) Emergency missile power off command (positive) Explosive switch fire command Explosive switch fired supervision Explosive switch installation supervision


Signal

J3-33 J7-34 J5-12 J7-35 J3-3, 2, 1 J3-32 J3-31 J3-41 J3-42 J4·10 J7-39 J7-38 J4-12, 13 J4-6, 7 J9-1 J9-2 J4-18 J4-36 J4-34

(

Connector pin(s)

{

09 89

HS

(

G17 F4, 04, E4 E6 06 87 C7 ES L17 K17 Nll A13 M21 A22

GlO

F6 F17



I

~

\

....~ '°

n

{

(, (

(

Signal

First stage actuator switch supply First stage actuator 1 oil temperature switch supervision First stage actuator 1 operating pressure supervision First stage actuator 1 precharge pressure and oil level supervision First stage actuator 2 oil temperature switch supervision First stage actuator 2 operating pressure supervision First stage actuator 2 precharge pressure and oil level supervision First stage actuator 3 oil temperature switch supervision First stage actuator 3 operating pressure supervision First stage actuator 3 precharge pressure and oil level supervision First stage ignition arm command

J13 J34 J22 H22 K34 L22 K22 M22 823 A23 LS

J9-23 J9-22 J9-24 J9-26 J9-25 J9-27 J9-30 J9·29 J4-23


J9·20 J9·21

Connector pin(s)


{


{

~

I

'

(

n

0

I'\)

.,.

First stage ignition command supervision First stage ignition fire plus First stage ignition fire zero First stage pump motor on command First stage separation command supervision First stage vane 1 position monitor First stage vane 2 position monitor First stage vane 3 position monitor Gimbal hot supervision Gimbal not cold supervision GSE lift·off relay return Guidance air supply temperature indication to power station Guidance compu ter cold supervision Guidance pressure monitor sw itch supervision Guidance program zero supervision Guidance section air supply temperature contro l


Signal

J3·28 J3·52 JJ.54 J8·16 , 17

J9·3 1 J9-44 J9 ·43 J4 ·21 J4 ·50 J7 .25 J7 ·2 6 J7·27 J8·34 J8·35 J9·5 J8 · 18 , 19

Connector pin (s)

M7 Nl6, N18

L7

AG

K9 M16 Al7 817 F20 G20 022 N17,Nl

JS

C23 C24 824



I

I

.,. N ...

~

(")

(

(

(

(

Signal

Guidance withhold command High energy initiator system high voltage monitor High energy initiator system not safe supervision Horizontal alinement switch supervision Horizontal alinement switch supervision supply Inverter on command Lift-off supervision Lift-off switch supervision Lift-off switch supply Long range program 1° limit supervision Long range select command Long range select supervision Missile power on indication Off select command Offselect supervision J6-23 J6-35

J4-10

J7-57 J9-54 J4-51 J8-8 JB-9 J4-14 J9-3 J9-52 J9-51 J5-30 J4-44 J7-54

Connector pin(s)

E14

H13

EB

F18

G9

Fll

C22 024 N20

FB

819 J13

F24 L9

Gl8



{


(

~

I

•

'

~

.l:lo

(")

N N

{I

(,.

(

Phase A Phase A, 26v ac 400 Hz Phase B Phase 8, (SRO preset motor supply) Phase 8, 26v ac 400 Hz Phase C Phase C, 26v ac 400 Hz Pitch attitude monitor Pitch attitude substitute command Pitch gyro torquer control phase Pitch pendulum output Pitch program 1 ° limit supply Pitch program zero command Pitch program zero supervision Positioning signal excitation Program generator hold command Regulated generator 1 return (-D) Regulated generator 1 + 28v de ( + D11)


Signal

J4-58 J6-11 J4-59 J3-59 J6-48 J4-60 J6-l 7 J7-5, 6 J7-11, 12 J8-25, 26 J8-47, 48 J5-26 J5-22 J5-29 J2·52 J4-35 J4-2 J4·12

(

Connector pin(s}

f

N12 Nll

C3 C9

Ell

MlO

011

(

C21, 021

Ll9, Ml9

K16, Ll6

Ml5, Al6

88

C15 NlO

N9 N8

Hl2

E12



~

I

\

w

N

..

-n

{

{

(

(

Signal

Regulated generator 2 retu. n ( -D) Regulated generator 2 + 2Bv de ( + D21) Return -DlO (monitor) Return -D20 (monitor) Roll attitude monitor Roll attitude substitute command Roll gyro torquer control phase SA integrator stop command SAD hold command SAD monitor and substitute command SAV hold command SAV monitor (SI, S2) SAV monitor and substitute command SAV offset command SAV switch supervision SAV zero command Second stage actuator switch supply

J3-51 J3-34 J9-32

J7-37 J3-35

J3-6, 5

J3-50 J3-36 J7-36 J3-55, J5-11

JB-51, 52

J4-15 J7-l, 2 J7-7, B

J4-4 J4-6 J4-1

Connector pin(s)

Fl3 Al3 CB GB Bl6,Cl6 Fl6,Gl6 G21, H21 J7 J6 Hl7 AB, FlO H4,G4 Jl7 H6 K7 G6 N20



(


(

~

I

'

\

n

fl,)

• •

Second stage actuator supervision Second stage actuator supervision Second stage actuator oil level supe rvision Second stage actu ator supervision Second stage actuator supe rvision Second stage actuato r oil level su pervi sion Second stage actuato r supervision Secon d stage actuator supervi sion

F23

G23 J23 H23

J9.35 J9·34 J9·36 J 9·38 J9·37 J9·14 J9·40

1 operating pressure

1 precharge pressure and

2 oil temperature switch

2 operating pressure

2 precharge pressure and

3 oil temperature switch

3 opera ting pressure

L23

F22

E23

023

)


J 9·33

-

Connector pin( s)

1 oi l temperatu r e switch


Signal


I

c.n

~

olao

-n

( {

( (

Signal

Second stage actuator 3 precharge pressure and oil level supervision Second stage pump motor on command Second stage vane 1 position monitor Second stage vane 2 position monitor Second stage vane 3 position monitor Select supervision supply Servoampl ac power on command Servoampl de power on command Short range program 1° limit supervision Short range program reverse command Short range select supervision Signal common ground Simulated first stage separation command SRO coarse (Sl, S2, $3) SRO fine (Sl, $2, S3) SRO hold command

M23 K8 Cl7 017 E17 Ll2 KlO LlO JlO Cll El8 Hl8 J9 H5, G5, F5 MS, E4, l5 ElO

J4-22 J7-28 J7-29 J7-30 J6-15 JS-20 JS-21 J5-19 J5-25 J7-53 J7-60 J4-48 J3-21, 20, 19 J3-27' 26, 25 JS-10


J9-41

Connector pin(s)


(


(

~

I

'

.i:.

(")

°'

~

.,.

{

{

(

SRO medium (Sl, S2, S3) SRO presetting motor control phase SRO release command SRV coarse (51, 52, 53) 5RV fine (51, 52, 53) 5RV hold com ma nd 5RV medium (51, 52, 53) SRV monitor (Sl, 52) 5RV motor control SRV presetting motor control phase SRV release command ST-120 air pressure switch supervision ST-120 base plate temperature supervision ST-120 base plate temperature supervision supply 5t-l 20 heater control 5T-120 heater control relay supply


Signal

JS,85,KS 07, E7 86 L4, G5, M4 E5, E4, 05 010 A5, 85,C5 K4, J4 K6 M6, A7 f7 H20 L21 Jl3 E20 f 19

{ {

{


J3-22, 23, 24 J3-43, 44 J3-29 J3-10, 11, 12 J3-18, 17, 16 J5-9 J3-13, 14, 15 J3-9, 8 J3-37 J3-39, 40 J3-45 JS-36 JS-56 JS-57 JS-33 J8-42

Connector pin(s)


/'

I

•

\

N ...,

..

n

( {

( (

Signal

Surface select command Surface select supervision Switch point 1 command supervision Switch point 2 command supervision Switch point 3 command supervision Synchrotransmitter on command T-pot release command Tail plug relay command Tail plug relay command supply Tail plug relay supervision Theodolite lamp fixed Theodolite lamp variable Thrust termination and second stage separation command supervision Umb'ilical release supervision Uncaged supervision Vanes locked supervision

I

M9 J19 L34

J4-54 J8-22 J9-57

I

C13 L13 818 C18 018 C6 L6 N19 N19 A24 F2,G2 F2, G2 E9


J6-19 J6-28 J7-50 J7-51 J7-52 J3-30 J3-38 J9-49 J9-50 J9-42 J2-19, 20 J2-19, 20 J4-40

Connector pin(s)


(


{

~

I

'

~

~

(")

co

N

(!

{'

(

Vanes unlock command Warhead continuity supervision Warhead continuity supervision supply Warhead signal withhold command Warhead signal withhold relay supervision Warhead 1 coarse ($1, $2, $3) Warhead 1 fine ($1, $2, $3) Warhead 1 release command Warhead 1 servomotor control phase Warhead 2 coarse ($1, S2, 53) Warhead 2 fine ($1, $2, S3) Warhead 2 release command Warhead 2 servomotor control phase Warhead 3 coarse (Sl, $2, $3)


Signal

{

J5-40 J6-5 J6-3 J9-39 J9-18 J6-24, 51, 43 J6-45, 44, 12 J6-46 J6-56, 57 J6-9, 30, 31 J6-53, 8, 10 J6-34 J6-32, 33 J 6-49, 58, 50

Connector pin(s)

(

{

Gll Cl2 812 K23 G22 Kl3, 85, Ml4 Al5, E4, Jl2 815 Jl5, Kl5 Fl2, 85, Al4 Gl5, E4, Gl2 014 814,Cl4 015, 85, El5



~

I

\

co

N

_,.

n

(

( (

(

Signal

Warhead 3 fine ($1, $2, $3) Warhead 3 release command Warhead 3 servomotor control phase Warhead 4 coarse ($1, $2, $3) Warhead 4 fine ($1, $2, $3) Warhead 4 release command Warhead 4 servomotor control phase X, Y, and Z gyro torquer constant phase (ph A and C) Yaw attitude monitor Yaw attitude substitute command Yaw gyro torquer control phase Yaw pendulum output 115v ac, 400 Hz platform heater supply (l20) 115v ac 400 Hz platform heater supply (neutral) 41 38

38 60, 55 21, 42

36, 16

J7·3, 4 J7-9, 10 J8-49, 50 J8-45, 46 J8-39 J8-40

J6-14, J6-59 J6-37, J6-52, J6-22, J6-39 J6-40, J8-37,

Connector pin(s)

016, E16 H16,J16 E21, F21 A21, 821 K19 N28

Kl2, E4, M12 L15 F14,G14 F15, 85, H15 Gl3, E4, L14 H14 J14, K14 J20, K20


Table 4-6. Signals on Con.nector Pins of PTS Cable Entry Panels-Continued

(


(

~

I

I

'

.,..

0

n

w

(

Missile power on command

Power Cable Entry Panel (A4A3)

- 2 5v de power su pply +28v de +010 monitor + 28v de + 020 monitor

+ 25v de power supp ly

(


Signal

JG -19

J7-39 J7 -38 J4-10 J4-9

Connector pin(s)

J27

ES 08

Kl7

Ll 7



I

Table 4-7. Power Distribution Buses

Bus Adapter (32A2) + 01 03 ( +28v dc) Power Distribution Assembly (32A6) - 0100 ( 28v de retu rn ) + 0101 ( + 28v de) + 0102 ( +28v de) + 010 3 ( +28v de) + 0300 ( + 24v de) + 0301 ( + 24v de) + 0 305 ( + 24 / 28v de) Ll 2( 120vac) L22 ( 120vac) L32 ( l 20v ac) Neutral + 12v de -12v de

,....,,

Sig nal Distribution Box (32A8) + 0201

Location

Connector pin (s) on power cable entry panel (A4A3)

TB 9-3 , .4

See note.

TBl l · l thru .4 TBll -7,·8 TB10·8 th ru -10 TBl 1·9, ·10 TB9 ·4, .5 TB9 ·8 thru · 10 TB8 - l

J4·E, F

TB3·8 TB3-9 TB3·10 TB2·7 thru .10 TB6·3 , -10 TB6·9

I

J 5. 1 J 5.2 See note. J5-6 J5·6 J 5·6, J5·1 J4·A ( LlO) J4-B ( l 20) J4-C ( L30) J4-D See note. See note .

I A2

J6·20

Note. Hardwired directly to adapter power supp lies.

C4

4-31

4-5 . Adapter Diagnostic Test Modes.

I WARNING

I

All jumper caps must be removed after performing the test modes listed below. Fai lu re to remove the jumper caps prior to initiation of a coun t· down with a live missile may result in injur y to pe r sonnel or damage to equipment.

a. Mode 00. PTS tactical, with azimuth laying control box and remote firing box. b. Mode 01 . PTS tactical , without azimuth laying control box and remote firing box. c. Mode 02. PTS with guidance section in.container . d. Mode 03. PTS with first stage in.container . e. Mode 04. PTS with second stag e in -con ta iner.

f. Mode 05 . SCTS with tactica l jumper caps.

I

g. Mode 06. SCTS guidance section with jumper caps (in con· tainer) . h. Mode 07. SCTS guidance section with jumper caps (in van). i. Mode 08. SCTS first stage with jumper caps. j. Mode 09. SCTS second stage with jumper caps.

4-32

C4

w w

,,.

nw

(

(

Test cable entry panel 32A4A2 (PTS) or 95A32A4A2 (SCTS)

07

06

05

04

03

02

01

00

R

R R

R

R R

R

IG

y

y

y

y

y

B

G G G G G G G y y y y y y

y

w w w w w w w w w

R

B

0 y

y B

y

0 0

y 0 y

y 0

x

J56 thru J65

x

60Wl8 and RFB

J6

Pneu. test console

( Fire control entry panel 32A4A5

Table 4-8. Jumper Cap Information

Tactical cable entry panel 32A4Al (PTS) or 95A32A4Al (SCTS)

(

Mode J2 J3 J4 JS J6 J7 JS J9 JlO J1 J2 J3 J4 JS J6 J7 JS

(

60W44 and ALCB

J2

Tactical cable entry panel 32A4Al (PTS) or95A32A4Al (SCTS)

{

~

I

~

n w

•w • Test cable entry panel 32A4A2 (PTS) or 95A32A4A2 (SCTS)

(

G - green

B - blue

Color code:

08 09

(

{

0 - orange R - red

B

0

B

0

0

0

W - white or aluminum Y - yellow

B

Mode J2 J3 J4 JS J6 J7 JS J9 JlO J1 J2 J3 J4 JS J6 J7 JS

Tactical cable entry panel 32A4Al (PTS) or 95A32A4Al (SCTS)

(

J6

Pneu. test console JS& thru J65

(

(

J2

Tactical cable entry panel 32A4Al (PTS) or95A32A4Al (SCTS)

X - no color designation

Fire control entry panel 32A4A5

Table 4-8. Jumper Cap Information-Continued

~

I

\

.,.

en

;,,

(

39.1 IN. ( 1.00 M)

SI

(

(

•\ IN. (0.32 M) _ _ _ _ _ 80.25 IN. (2.04 M) TOW POINTS OR TIEOOWN POINTS 11,600 LB (5,261.76 KG) EACH (TYP, BOTH SIDES) FSNB-14

.112.6

81.5 IN. (2.07 M)

\ ·~1J

L•4.0 IN._.j• (0.86 M)

~

DI

n

(

TIEOOWN POINTS 11,600 LB (5,261.76 KG) EACH (TYP, BOTH SIDES) ~HOIST POINTS

Figure 4-1. PTS shelter physical data.

96,0 IN. I (2.44 M) ,. 98.5 I N · - - - - - - . . i NOTE: (2.50 M) WEIGHT: 4,291 LB (1,948 KGt

I

(

HOIST POINTS 11,600 LB (5,261.76 KG) EACH (TYP, BOTH ENDS)

(

_,)

w

n

°'

~ w

(

(

(l.79 M)

70. 3 IN.

{

00

139.0 IN, (3.53 M)

(

{

(

FSNB-13C.

I

95.0IN.~

(2.41 M)

r

Figure 4-2. PTS-PS transportation data.

NOTES: 1. WEIGHT: 24,747 LB (11,225 KG). 2. AXLE LOADS: C & D-5,878 LB (2,667 KG) EACH. E & F-6,495 LB (2,943 KG) EACH.

)

"\

17

15

FSNB-31

'W

.,,.,

._,

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17

-

Remote firing box Azimuth laying control box Air duct register Phone control panel assembly Adapter Storage cabinet Card and module test set Power distribution assembly Power distribution assembly circuit breaker panel Signa I distribution box Computer box front access panel Computer box top access panel Computer Air filter First aid kit Blower Storage cabinet Fig ure 4-3. PTS interior, left side.

4-37

cii

"O

...

'iii .r:.

bD

·;:

..: 0

·;: Q)

c

...::I Q)

bD

il:

4-38

Cl

-

'°

w

~

n

I

1 2 3 4 5 6 7 8 9 10 11 12 13

{

-

(

Figure 4-4. PTS interior, right side -

Launch control panel assembly Maintenance panel assembly Storage cabinet Utility panel assembly Utility circuit breaker panel assembly Air duct register Teleprinter , Tape storage cabinet Air conditioner Air supply register Air conditioner filter Air conditioner control panel Remote firing box cable reel assembly (travel position)

(

-

{

(

Storage cabinet Convenience outlet (4) Auxiliary heater Workbench Signal distribution box Blower Console Voltage-phone monitor panel assembly Countdown control panel assembly Azimuth laying control panel assembly Tape reader Hand lantern

Legend.

14 15 16 17 18 19 20 21 22 23 24 25

(

~

'

r

CHAPTER 5 POWER STATIO N (CONTENTS) Item PS enclosu re, right fron t ................. . PS shelter physica I data ................. . . Tabulated data ............................... .

Reference Fig. 5 -2 Fig. 5 · l Par. 5-1

Page

5.7

I

5-6

5.3

II

Cl

5-1

CHAPTER 5 POWER STATION 5-1 . Tabulated Data. a. General. Max tilt angle: Operation ........ .............. ......................... ..... ...... ....... 6 ° Shipment ...................... .. ...... ... ... .. ..... .. .............. .... 30° Temperature where conditioning set is needed .................................. Below -3 1.7 ° C (-25°F) Max operational altitude .. ............... ...... 8,000 ft (2438 m) Convenience receptacle power ...................... l 20v, 400 Hz b. Gas Turbine Engine. Governed speed ................................ 42,000 rpm ( 100%) Overspeed shutdown .................................... .... 1 10% rpm Ma x exhaust temperature: Operating ....................................................... 64 0°C (l,184°F) Shutdown (normal) ............................................. 460 °C (860 °F) Shutdown (emergency ) .... .............. ......... ....... 720 °C ( l ,328°F) Electrical system: Operating ....... ... ............ ............. ....... ....... .............. 28v Starting ............. ........ ..... ... ...... ... ..... .... ..... ... ... ..... ... 24v Operating oil pr essure: Engine ................................................... 80 to 100 psig Gearbox ................................................... 15 to 50 psig Gearbox oil filter bolt torque .... .. .. .. .... .. .... .. .. 36 to 70 in.-lb Low oil pressure lamp indication: Engine ........................ .. ........................... 27 to 30 psig Gearbox ......................................................... 9 ± 1 psig c. Air Conditioner. Airflow to missile (sea level) .............. 37 .6 ± 2.6 lb per min Discharge pressure .. .................. .... .................. 2 to 5 psig Bleed air duct, clamp bolt torque .......... ... .. .. 60 to 70 in.-lb d. AC Gener ato r. Speed .... ..... .... ... ... ...................... .. ... .... ... .. ...... 6,000 rpm Rating: KVA ................. .. ..................................... .40 at 0.75 pf Voltage ................. .. ........................ ........ ...... . 120/ 208 Frequency ... ..... .... ....................... ...... ........ ........ ... 400 Hz Pha ses .................... ..... .... .. .. .. ... .... ..... .. ... ..... .. ..... ......... 3 Type of connection ........................................... 4 -wire wye

C4

5-3

I

Lamp indications: Overvoltage ................................................ 16 2 to 17 6v Undervoltage ................................................. 53 to 67v Underfrequency ................................................. 373 Hz ~

e. DC Generator. Speed ............................................................. 6,000 rpm Rating: Voltage ....................................................................30 Amperes ................................................................300 Lamp indication, overvoltage ............................ 35.5 to 39v Undervoltage disconnection .................................. 7 to 1 lv

~

f. Air Compressor.

I

Nominal discharge pressure ............................. 3,000 psig Speed .............................................................4,000 rpm Lamp indication, low oil pressure ..................... 20 psig min

g. Instant Air System Cylinder. Nominal pressure ............................... 2,900 to 3,000 psig Volume ............................................................... 1.5 cu ft Pressure rating ................................................ 3,600 psig·

h. Battery (2). Type ........................................................ Nickel cadmium Rating: Voltage ............................................. 12 (single battery) 24 (series connected batteries) Ampere-hours .......................................................... 70 Cells ........................................................................... 10 Electrolyte .......................... Alkaline (potassium hydroxide) Weight (filled) ............................................. 80 lb (36 kg) Limiting charge: Voltage .................................................... l.55v per cell Current ............................................................40 amp

i. Battery Charger.

I

Power: Input ................................. 120/208v, 3-phase, 400 Hz Output .................................................. 28v de, 35 amp

5.4

C3

\_.I

r j. AC Voltage Regulator. ·voltage adjusting range .................................. 200 to 218v k. DC Voltage Regulator (2). Voltage adjusting range ...................................... 25 to 35v ~IC •• • apac1t1es.

~

Fuel tank ..........................................................82.25 gal Engine oil tank ......................................................... 1 gal Gearbox oil sump .................................................... 1.7 qt Air compressor oil sump ............................................. 3 pt

5.5

w

n

°'

UI

{

{

91 IN.(2. 31M) X 4 IN.(O. lOM) ( TYP, BOTH SIDES)

BEARING SURFACE

U

30.GIN. (0.78 M)

LEFT SIDE

TlEDOWN POINT (TYP, BOTH SIDES)

~ fl

----~AFT

~~E

I

~

LIFT

(.

~

/

(

Figure 5-1. PS shelter physical data.

('

(,

32. 0 IN.. _ . (0.81 M) FSNB-24B.

~l.5Di) (0.04 Ml

~

Mf-,

u:::I::

F(l.02

j_2s (o:oa Ml

3 OIN

J ~rn:>

42.381N.

( 1.08 M)

' - - - 40. 0 IN-----.1

L1

AFT OUTBD DOWN 10, 000 2,650 10,000 (4, 536) (1, 202) (4,5361

1. GROSS WEIGHT: 4,030 LB ( 1,828 KG). SKID HGT 2. NET WEIGHT: 2,692 LB (1,221 KG).

Ii

~OTES:

~

(2.3131

FWD 5,100

MAX TIEDOWN LOADS IN POUNDS (KILOGRAMS)

~

"\

......

\II

.

n

(

ELECTRICAL DISTRIBUTION CENTER

HlGH-PR ESSURE Ara DISTRIBUTION PANEL

VENTILATION INLET DOOR

HORN OPENING

(

(

Figure 5-2 . PS enclosure, right front.

(

AIR COMPR ESSOR OIL FILLER ACCESS DOOR

FSNB-49 I

-

'-'

CHAPTER 6 AZIMUTH LAYING SET (CONTENTS) Item

¥

Azimuth laying equipment ................ . Equipment container 1 .................... . Equipment container 2 .................... . Tabulated data ............................... . Theodolite scale reading .................. . Theodolite scales ............................ .

Reference

Page

6-1

6-5

6-3 6-4

6-1

6-7 6-8 6-3

6-2 6-2

6-6 6-6

Fig. Fig. Fig. Par. Par. Fig.

•

6-1

r

CHAPTER 6 AZIMUTH LAYING SET 6 - 1 . Tabulated Data. a. Battery Box. Refer to TM 5·6675 -296· 12 or TM 5·6675·1 296·35 for data regarding the battery box. b. Bed Assembly. Length ......... ................... .............. 33-3/ 4 in. (85.73 cm ) Width ...................... ...... ...... .. .. .... ... . 9 -1 / 4 in . (23.50 cm) Height ....... ...... ..... ..... .... .. ....... ........ 6-112 in. ( 16.51 cm) Weight.. .... ....... ... ................... ........... .. ..... 22 lb (9 .99 kg)

-

c. Control Box (Stored in PTS) . Len gth ....................... .... ...... .... .. .... ..... ... 9 in. (22.86 cm) Width .. ............... .... ..... .. .. ............. ... 6-3 / 4 in. ( 17 . 15 cm) Height ......... ...... ......... .... ........... ... 5-3 / 64 in. ( 12.82 cm) Weight. .. .. ... .. .. ... .. ............. ............... ... ... .... 6 l b (2.72 kg) Power requirements ............ ................ l 15v, 400 Hz, and 28v de d . Equipment Container 1. Len gth .... .. ................... .... .. ... ................ 43.1 in . (l.09 m) Width ..... ........ ................... ... .. ....... .. .. 28. 1 in. ( 71.37 cm) Height ........ .... .. ... ....... .... ......... .. ..... .. 23.2 in . (58.92 cm) Weight (empty) .. ........................ ..... .. 162.8 lb (73.84 kg) Weight (loaded) .................... ....... .. .... 287 lb (130. 18 kg) e. Equipment Container 2. Len gth .................................................. 43.1 in. (l.0 9 m) Width ................. .. .......................... .. . 28.l in. (71.37 cm) Height .......................... ..... .............. .2 3.2 in. (58.92 cm) Weight (empty) ......................... ........ 109.9 lb (49.85 kg) Weight (loaded) ........... ......... ...... 238-2 / 3 lb (108.36 kg)

f. Head set-Microphone Assembly. Length ..... ........... ... .. ... ....... ... ...... ... . 6-1 / 2 in. (16.51 cm) Width ....................... ......................... 3 -5 / 8 in. (9.2 1 cm) H eight (retracted) ..... .... ............ .... ......... 9 in. (22.86 cm) Cable length .............. ............. ...... ... ... .... ... 19 ft (5.7 9 m) Weight ............. ............................................. 2 lb ( 90 7 g)

C4

6-3

I

g. Illuminated Sunshade Assembly. Note All dimensions and weights are approximate. Length .....•.........•.•............................... 10 in. (25.40 cm) Width (with adapter plate) ................ 5·3/8 in. ( 13.65 cm) Width (without adapter plate) .................... 3 in. (7.62 cm) Height ............................................ 5·1/4 in. (13.34 cm) Weight (with batteries) .................................. 1 lb (454 g)

h. Metal Tripod. Length (legs retracted) .................. 35·1/4 in. (89.54 cm) Width (tripod head) ....................... 14·5/8 in. (37.15 cm) Height (tripod head) ...................... 13·1/2 in. (34.29 cm) Weight .................................................. 46 lb (20.86 kg) i. Target Set Carrying Case With Contents. Length .......................................... 12.114 in. (31.12 cm) Height .......................................... 10·1/2 in. (25.73 cm) Depth ............................................. 6· 1/8 in. ( 15.56 cm) Weight. ........................................................ 2 lb (907 g)

I I I

I

j. Theodolite. Refer to TM 5·6675·296·12 or TM 5·6675·296· 35 for additional data regarding the theodolite. Telescope ..................................................... 28X (power) Shortest focusing distance ......................... 4.5 ft ( 1.37 m)

Longest aiming distance at which centimeter can be read ........................................ 1,000 ft (305 m) Longest aiming distance at which mil can be evaluated .............................................. 465 ft ( 142 m) Normal range ............................. 6 to 12 mi ( 10 to 19 km) Accuracy of circle readings .........................................• 0.001 mil Multiplication constant ......................................................... 100 Addition constant ..................................................................... 0 Graduation interval of horizontal circle ...................... 0.002 mil Weight .................................................... 12.3 lb (5.6 kg) Carrying case ............................................ 4.8 lb (2.2 kg)

k. Theodolite Sunshield Tent Assembly. Length ..................................................... 74 in. (l.88 m) Width ...................................................... 74 in. ( 1.88 m) Height ..................................................... 76 in. ( 1.93 m) Weight ................................................. 69 lb (31.30 kg) I. Tripod. Refer to TM 5-6675-296-12 or TM 5·6675-296·35 for additional data regarding tripod T2. Length extended ......................................63 in. (160 cm) Length folded ...................................... 38.5 in. (97.8 cm) Weight .................................................... 14.4 lb (6.5 kg)

C4

ORlENTING STATION THEODOLITE (OST) ORIENTING LINE TARGET (OLT )

VERTICAL LAYING THEODOLITE (VLT) HORIZONTAL LAYING THEODOLITE (HLT)

A. AZIMliTH LAYING SET, MAJOR COMPONENTS

B . AZIMUTH LAYING CONTROL BOX FSNB - 23A I

Figure 6-1. Azimuth lay ing equipme nt.

Cl

6-5

6-2. Theodolite Sca le Read ing. The scales of the theodolite (fig. 6-2) are read by looking th rough the microscope eyepiece attached to the telescope. The horizontal circle illuminating mirror must be reflecting light into the theodolite. The inverter (circle selector) knob must be in the horizontal position for the correct ang le to be read. The whole.number portion of the scale is divided into two parts. The upper half appears inverted, and the scale readin gs are exactly 3,200 mils oppos ite the sca l e readings of the lower half. A scribe mark is set in the center of the lower scale. The first number on the lower scale to the left of the scribe mark 1s the number that is read for a direct reading. The first number on the upper half of the scales to the right of the scribe mark is 3,200 mil s opposite the number on the lower ha lf of the scales: this number is read for a rever se reading. The number of spaces is counted from the first number to the left of the scribe mark on the lower half of the scales to the first number to the right of the scribe mark on the upper ha lf of the scales. This number is the unit value that 1s combined with the number read from the lower hal f of the scales to give th e complete whole.number part of the direct scale readin g. (Th e graduation marks of the upper scale must coincide with the graduation marks of the lower sca le before a reading can be obtained.) The decimal part of the scale readings is read from a second small scale below the whole.number scales. This scale can be read to 0.002 mil. and must be interpolated to the nearest 0.001 mil. A reverse reading is a combination of the decimal reading and the whole-number reading from the upper ha lf of the whole.number scales.

DIRECT 207G. 2:;4 REVERSE ;)276. 2:;4

Figure 6-2. Theodolite scales.

6-6

F S:\B-:lli

CHAPTER 7 BATTERY CONTROL CENTRAL (CONTENTS) Item

Reference

Page

sec in terior, left side ..... ..... ....... ..... . sec interior, r ight side........... .. ....... . sec shelter physica l data· ············· ··· sec t ranspo rtatio n data·· ······· ··· ·······

Fig. Fig. Fig. Fig. Pa r. Par.

7-6 7.4 7.3

Gene ral ..................... ...................... ...... . Tabulated data ....... .......... .. ...... ....... .......

7.3

7- 2 7-1 7.4 7-1 7·2

7 -8

7·2.1 7·2.1

I

I

C4

7·1 /(7·2 blank)

CHAPTER 7 BATTERY CONTROL CENTRAL

I

7-1. General. The BCC provides a centralized facility for consolidation of all release communications and for batte ry command and control functions.

"-"" I

7-2 . Tabulated Data. a. Primary Power System. Traile r-mounted 15-kw generator, towed behind the vehicle for 120/208-volt, 3-phase, 60-Hz pow· er. Two 25v de power supplies. One 9v de power supply. b. Back·Up Emergency Power System . 24v de battery sou rce from the vehicle.

C4

7·2.1 /(7·2.2 blank)

·--

'-1

-

_____,·

( (")

""

HOIST POINT (TYP BOTH SIDES) (SEE NOTE 2)

.cu, ,v IN ....... 267.0 (6.78M)

HOIST POINTS (SEE NOTE 2)

(

I

DD DJ Dl

~ -···

"

' ~ .,...

•

39.7 IN. ( 1.01 M )

* 14---

99.1 IN. - - - (2.52M)

2-03.S '"

~

(5.17M)

....

--I

NOTES, 1. WEIGHT, 11,818 LB (5,361 KG). 2. TWO WRECKERS M543 AND TWO MULTI LEG SLINGS ARE REQUIRED WHEN LIFTING

acc.

FSNB-l CI

"w

Figur e 7 - 1. BCC shelter physical data.

n

.;..

...,

{

(

34

{

{

Figure 7 -2. BCC interior, right side.

22

(

{

FSNB-44A

I

~

'\

UI

......

n ...,

I

I

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

-

19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36

-

Figure 7-2. BCC interior, right side -

Remote firing box housing ( 3) PAL unit T-1500A mount (3) PAL unit T-1500A connector (3) Remote firing box connector ( 3) Electrical rack Power panel Test points Console FM transceiver 1 AN / VRC-46 Status display panel Clock Telephone TA-312/PT (TRC-133 A) Handset H-138/U (3) Radio set control C-2328/GRA-39 (3) Pa per transfer slot TRC-80 panel Chalk tray Loudspeaker LS-454/ U

(

Legend .

Magnetic chalkboard FM transceiver 2 AN / VRC-46 AM receiver AN / GRR-5 Desk tray 120v ac convenience outlet Chair (4) Security safe FM receiver R-422/VRC Intercom select panel Alert warning system switch Remote speaker console Removable brace Remote speaker console cable Telephone TA-312/PT (FIELD SWBD) File cabinet (four-drawer) First aid kit and mounting Fire extinguisher Wo rktable

I

.....

OI

(

Figure 7 - 3. BCC interior, left side.

FSNB-43

..... .:...

-

(

(

(

( {

Legend •

16 - Klaxon (3) and storage fixture 17 - Emergency lantern (2) and storage fixture 18 - Storage cabinet 19 - Ax 20 - Klaxon cable reel (3) and cables 21 - 25v de power supply 1 22 - 25v de power supply 2 23 - 9v de power supply 24 - Bifold table 25 - Antenna storage box 26 - Security safe 27 - File cabinet (two-drawer} 28 - Chair 29 - Klaxon tripod 30 - Typewriter

Figure 7-3. BCC interior, left side -

Pencil sharpener Patching switchboard l 20v ac convenience outlet Telephone switchboard SB-22/PT (2) Headset H-161 ( )/U storage bin (3) Recorder's control box (3) Radio set control C-2328/GRA-39 (3) Magnetic chalkboard Paper transfer slot Clock Chalk tray FM transceiver noise suppression cover (2) 13 - Blower unit 14 - Typewriter storage area 15 - (60Wl01) Ground cable (2)

1 2 3 4 5 6 7 8 9 10 11 12

(

~

l

~

•

.....

(

{

(

(

Figure 7 -4. BCC transportation data.

( 3.61 M)

(

(

FSNB-2C.

TIE DOWN POINT (PINTLE) 20,000 LB (9, 072 KG) LIMIT LOAD

lllIN.

981N.~

r---101. 0 IN. (4.75 M)

I _EXPA~DED WIDTH~

.,..._ _ _ _ _ _ _ _ _ _ 330. 0 I N . - - - - - - - - NOTES: <8 • 38 M) TIEDOWN 1. WEIGHT: 27, 190 LB (12,333 KG). (TYPICAL BOTH SIDES) 2. TURNING RADIUS: 42.5 FT (12.95 M). 15, 000 LB (6, 804 KG) FWD OR AFT 3. TWO WRECKERS M543 ARE RE40,000 LB (18,144 KG) INBD OR OUTBD QUIRED WHEN LIFTING BCC 8,500 LB (3,856 KG) UP OR DOWN · LIMIT LOAD

TIEDOWN AND HOIST POINT (TYPICAL BOTH SIDES) r-----.-----,'~'.lli.~oe-------,==::::::---1 ' \. 15, 000 LB (6. 804 KG)-' LIMIT LOAD

TIEDOWN POINTS (TYPICAL BOTH SIDES) 17,500 LB (7,938 KG) LIMIT LOAD

)

'\

CHAPTER 8 RADIO TERMINAL SET (CONTENTS) Item

""""

RTS shel ter physical data ................ . RTS transportation data ................... . Technical characteristics ................ ..

Reference

Page

Fig. 8-1 Fig. 8-2 Par. 8-1

8-5 8-6 8-3

I

8-1

r

r CHAPTER 8 RADIO TERMINAL SET

'wl 8-1. Technical Characteristics. a. General. Range: Non-diversity operation ........... 70 statute miles (113 km) Diversity operation ............... 100 statute miles (161 km)

~Azimuth:

Coverage ...................................................... 6,400 mils Shelter: Size (overall) ............................... 69 in. (175 cm) high, 80 in. (203 cm) deep '...,I Weight. .......................................... 4,764 lb (2,161 kg) Primary power .............................. 208v, 4-wire, 400 Hz Ambient temperature range: Operating .............. -25°F (-31.7°C} to 125°F (51°C) Storage .............. -65°F (-53.8°C) to 160°F (71.1°C) b. Transmitting System. Frequency .................................................4.4 to 5.5 GHz Channels .................................... 333 at 1.8-MHz intervals Type ·of modulation ...................................................... FM Power output ................................................. 1,000 watts

c. Antenna Assembly. Type .................................................................Inflatable Support ...................... Pressurized peripheral ring and collapsible aluminum frame and feed horn support arms '-..I Air pressure and source: Peripheral ring ....... 15 psi from motor-driven compressor Para bolo id bag ................ 4 psi from motor-driven blower Dimensions: Paraboloid reflector diameter ................. 96 in. (244 cm) Diameter including side support frame ........... 10 ft (3 m) Elevation above top of shelter ........................ 10 ft ( 3 m) Position (manual): Azimuth ............ ± 3,200 mils in 100-mil increments from roof of shelter; through 100-mil range ".._/ from operator's compartment Wind: Storage and transport... ... 80 mph (129 kmph} with gusts to 120 mph (193 kmph)

Cl

8-3

I

Assembly, disassembly, and operation ................... 40 mph (64 kmph) with gusts to 60 mph (96 kmph)

d. Communication Capabilities. Teletype circuits: 2-wire de: RTS operator, Army and fire control in 3-party loop Receiver teletypewriter output to fire control RTS operator and fire control in 2-party loop Voice frequency: 2-wire/ 4-wire, fire control to RTS radio 4-wire, RTS operator and Army 4-wire duplex, RTS operator and RTS radio Speech circuits: 2-wire between fire control and RTS radio or operator 2-wire intercom, fire control and RTS operator 2-wire/ 4-wire telephone, Army and RTS operator 4-wire plus keying line to vehicle radio 4-wire spare 4-wire between RTS operator and RTS radio

e. Power Unit.

I

Type ............................... Gasoline-engine-driven alternator Output ........ 10 kw, 12.5 kva, 120/208v, 3-phase, 400 Hz Fuel consumption ....................... 2-1/2 gph (9.5 liters/hr)

8-4

C3

~

~

~

CD

cit

(

(

(

., I

(

(

...

ti

LIFT POINTS (TYP, BOTH ENDS)

Figure 8-1. RTS shelter- physical data.

\

ALTERNATE TIEDOWN POINT (TYP, 6 PLACES BOTH ENDS)

-~~~~--+~~-

AFT-f-FWD

55. 0 IN. (l.40 M)

BEARING SURFACE 25. 0 IN. (0. 64 M) X 13, 0 IN. (0. 33 M) (TYP, BOTH SIDES) NOTES: l. WEIGHT: 4, 840 LB (2, 196 KG), 2. NOTE: MAX TIEDOWN LOAD: 15, 000 LB (6, 804 KG) IN ANY FORWARD DmECTION.

TIEDOWN POINTS (TYP,BOTH ENDS)

(

~

~

m

w

(')

0.

(

{'

AXLE F

(

AXLE D

e

(

Figure 8-2. RTS transportation data.

E

AXLE

NOTES: 1. WEIGHT: 22,030 LB (9,992 KG). 2. AXLE LOADS: C & D-5,226 LB (2,371 KG) EACH. E & F-6,428 LB (2,918 KG) EACH.

(

c

AXLE

~

(,1

FSNB-15B.

T

124.75 IN. (3.17M)

)

'

CHAPTER 9 CABLE DATA (CONTENTS) Item

...,,

Air pressure test setup ..................... Air tern peratu re test setu p ................ Azimuth laying control box test cabling data ................................. Cable data ....................... ....................... Cable mast cable test conn ections ....... Cabl e transport or storage area data ............................................ Connector pin number-to-letter cross-reference .... .... ..... ............... EL electr ical circuit test set cabl ing data .................................... ........ Firing position auxiliary power cabl ing data, one missile .......................... Fi r ing position cabling data ...... .. .. ..... Fi rst stage in-conta in er test cabling data ............................................ Fi rst stage in-container test cabling data, using PSE ............................ Guidance section in-container heat cabl ing data ................................. Guidance section in-container test cabling data ......... .............. ...... .... Guidance section in-con tainer test ca bling data, using PSE .... ..... ........ Guidance section in-van cab ling data ............................................ Guidance section pressure test ......... Headquarters battery cabling data ..... Interstage electrical cable connections ...... .................. .......... Missile in-container heat cabl ing data .. .......................... .............. .. Missile in-container test cabling data ... ........ .... ........ .. ...... .. .......... . Missile in-container test cabling data, using PSE ........... .. ....................... Preparation for standby cabling data, one missile .... .. ........ ............ Prepa ration for travel cabling data .... Pressure switch test setup ...... .......... C4

Refe re nce

Page

Fig. 9-4 Fig. 9.5

9-4 1 9-42

Tab le 9-18 Table 9-27 Fig. 9- 1

9-28 9.51 9-20

Table 9-25

9.43

Table 9-24

9-43

Table 9 -11

9-19

Tab le 9.4 Tabl e 9-2

9-9 9-5

Table 9-15

9-24

Table 9-20

9.32

Table 9-10

9-18

Tabl e 9-17

9-27

Table 9-22

9.35

Table 9-23 Fig. 9-2 Table9-12

9-38 9.39 9-21

Table 9-3

9-8

Table 9.9

9 -17

Table 9-14

9-23

Table 9-19

9.30

Table 9.5 Table 9-8 Fig. 9-3

9-10 9- 1 5 9-40

9 -1

I

I

(CONTENTS- CONTINUED) Item

I

QRA auxi l ia ry and sta nd by power cab ling da ta , three mi ssiles ... ....... . QRA standby cabling data , two missiles ............ ....... ............ ..... .. . Reference desig nations ...... ... .......... . RFI cables .............................................. SCTS cabl ing data , using PSE ............... . Secon d stage in -con tainer te st ca bl ing data ........................................ . Second stage in -container test cabling data, using PSE ........... ........... .

'Ty:i~~~l ri~~ll~~g~edsu.~t·~·~········· ············· ····· Use of tables ................. ................... ..... .

9-2

Reference

Page

Tab le 9-7

9- 13

Table 9-6 Table9- l Table 9-26 Table 9-13

9-11 9 .3 9-50 9-22

Tab le 9-16

9-26

Table 9-21

9.34

Fig. 9·6 Par. 9-1

9.57 9.3

C4

r CHAPTER9 CABLE DATA 9-1 . Use of Tables. a. General. For commonly used abbreviations, refer to chapter 1. For cabling diagrams, refer to TM 9-1430380-14.

'-'1

b. Cabling Data Table Columns. ( 1) The "Cable" colunin lists the cable reference designations in numerical sequence.

~

( 2) The "From" column lists cable connector terminations. For example, "Pl (2) to PTS - A4A2J6" indicates that plug 1, . with indexing sleeve keyed at position 2, is connected to the PTS at J6 of the test cable entry panel (A4A2). ( 3) The "To" column lists cable connector terminations. For example, "P2 (5) to 2nd stg cntr - W6J6" indicates that plug 2, with indexing sleeve keyed· at position 5, is connected to the second stage container at W6J6.

Table 9-1 • Reference Designations Reference designation

Assembly

PTS A4Al A4A2 A4A3 A4A4

A4A5

Tactical cable entry panel Test cable entry panel Power cable entry panel Communications cable entry panel Fire control cable entry panel

A22 A26

Receptacle box (utility panel) Electrical distribution center

Al Al AS

Control box chassis (cQntrol unit) Heating blanket junction box (guidance and warhead sections)

PS

EL

9.3

r

Table 9-1. Reference Designations-Continued Refere nce designation A9

AlO W2

Assembly Heating blanket junction box (propulsion sectio n s) Intercommunications box (intercom box) Eme rgency power cable

SCTS

A32A4A l A32A4A2 A32A4A3 A32A4A4 None

Tactical cable entry panel Test cable entry panel PTS power cable ent,.Y panel Commur:iications cable entry panel SCTS POWER entry panel (i nput power)

-

9-4

'°u.

-n

(note 5)

(note 3) (note 4) (note 4)

(2) ( 3) ( 1) (7) (5) (4) (6)

(

From

P2 P2 P2 P2 P2 P2 P2 P2

P2 P2 P2 P2 P2 P2 P2 P2 P2 P2

(

To

(

(4) ( 1) (F) (8) (F)

to PTS · A4A1J9 to PTS · A4AlJ7 to 1st stg . JlO to PTS · A4AlJ6 to headset

(F) to 10-kw gen . WlJ 1 (F) to EL · A9J2 (F) to EL · A9Jl

(3) to EL · AlAlJ 1 (3) to PTS · A4A1Jl0 (1) to PS· A26J6 (9) to PTS · A4A1J8 or AlA1J5 (note 1) ( 13) to PTS · A4A1J4 (7) to PTS · A4A 1J5 ( 14) to PTS · A4AlJ3 ( l) to PTS · A4A3J2 ( 10) to PTS · A4A3J 1 (2) to PTS · A4A5J6

Table 9-2. Firing Position Cabling Data

{

to PS· A26J2 to EL · A 1A lJ 2 to CM A • J 6 to CMA · J2 to CMA · J4 to CMA ·JS to CMA · J3 (F) to PS· A26J5 (F) to PS· A26Jl (2) to BCC · J5 (or J7 or J9) or RFB · J 1 (note 2) Pl (4) to EL· W2Jl Pl (F) to 2nd stg blanket· J 1 Pl (F) to 1st stg blanket· Jl Pl (F) to 1st stg · Jl P 1 ( 2) to CM A · J 7 Pl (F) to EL· A9J3 Pl (3) toCMA· Jl Pl (F) to EL· AlOJl

Pl P1 P1 Pl Pl Pl Pl Pl Pl Pl

{


60W21 60W25 60W25 60W32 60W34 60W38 60W40 60W43

42W50 42W54 60W3 60W9 60Wl0 60Wll 60Wl2 60Wl6 60Wl7 60Wl8

Cable

(

~

I

'

N

n

°'

'°

(

(

{

Pl (F)toM656 Pl ( l) to 10-kw gen· W2J2 Pl (F) to WS blanket· J2 P 1 ( f) to GS blanket · Jl Headset (f) Headset ( F) Headset (F) Headset (f) Headset (F) Headset (f)

60Wl08 (note 3) 60Wl09 (note 8) 60W114 (note 4) 60Wl15


Pl (F) to ALCB · Jl GRD (F) to PS· GRD GRD ( F) to EL · grd panel GRD (f) to EL· grd panel GRD (F) to grd rod 1 Pl (F) to PS· A22J4 Pl (1) to CMA ·JS

From

60W44 60Wl01 60Wl01 60Wl01 60Wl01 60Wl03 (note 6) 60Wl05

Cable

To

{

('

(1

P2 ( 15) to PTS · A4A1J2 GRD (F) to PTS · A4A4J8 GRD (F) to PTS · A4A4J7 GRD ( F) to grd rod 1 GRD (F) to grd rod 2 P2 (F) to vehicle M656 P2 (F) to BCC · Jl (or J2 or J3) or 1500A. J3 (note 7) P2 ( 1) to PTS · A4A3J3 P2 (3) to PS · A26J7 P2 (f) to EL · A8Jl P2 (f) to EL · A8J2 RFB - J2 RFB - J3 PTS · A4A4J4 PTS · A4A4Jl PS· A26J4 ALCB · J6

Table 9-2. Firing Position Cabling Data-Continued

r.

~

1

I

'\

'°.:..,

n ...,,

(

Headset (F) Headset (F)

PS PS

(

(

From EL· AlA1J3 60W43 P2 (F) CMA Cfv1A

Table 9-2. Firing Position Cabling Data-Continued

{

To

(

I

I

'

~

Notes: 1. Alternate connection for ST-120 in-transit or standby heating. 2. Alternate connection for remote firing box external usage. 3. Connection for in-transit heating of programmer test station. 4. Used when ambient temperature is -32°C (-25°F) or below. 5. Used when ambient temperature is - 7°C (20°f) or below, and for 30 minutes prior to starting power station at -32°C {-25°f) or below. 6. Used for emergency starting of power station. I 7. Alternate connection for T-1 SOOA external usage. 8. Secondary usage (power station battery charging).

Air duct High-pressure airhose

Cable

(

Table 9-3. Interstage Electrical Cable Connections From 1st stage

llWlPl 11 W2P2

11W3Pl 2nd stage

To 2nd stage

10W1J2 10W2J2 10W3J 2 Guidance section

lOW l P l 10W2Pl 1OW3P1

8Wl9J3 8W20J 3 8W24J 2

Guidance section

Warhead section

7W l P2 7W3 Pl

9-8

4W36J8 4W l 18J2

ID ID

n

Pl ( 2) to PS· A26J2 Pl ( 1 ) to 45-kw gen · J8 Pl (F) to PS · A26J5 Pl ( F) to PS· A26J 1 GRD ( F) to PTS · A4A4J 8 GRD (F ) to PTS · A4A4J7 GRD ( F) to EL · grd panel GRD (F) to grd rod 1 GRD (F) to 45 -kw gen · GRD GRD (F) to PDB · J l2 GRD ( F) to grd rod 1 Pl (1 ) to PDB · J9

From

Notes: 1. Cables install ed as part of normal firing position in stallation. 2. Two groun d clamp assemblies are required at this location. 3 . Primary usage (standby power). 4. Basic signa l and winterization cables not included .

42W50 ( note 1) 58Wl 60W 16 (note 1 ) 60W 1 7 (note 1 ) 60W l 01 ( note1) 60W l 01(note1) 60W 10 1 (note 1 ) 60Wl0 1 (note 1) 60W 101 60W 10 1 60W 101 60W 109 (note 3)

Cable

P2 (3) to EL · A l AlJl P2 ( 1) to PDB · J 1 5 P2 ( 1) to PTS · A4A3J2 P2 ( 10) to PTS · A4A3J 1 GRD (F ) to PS · GRD GRD (F) to EL · grd panel GRD (F) to g rd rod 1 GRD ( F) to grd rod 2 GRD (F) to grd rod 1 (note 2 ) GRD ( F) to grd rod 1 GRD (F) to grd rod 2 P2 (3) to PS · A26J7

To

Table 9-4. Firing Position Auxiliary Power Cabling Data, One Missile

(

I

.s:i.

(')

0

'°. ....

P 1 ( 5) to CMA · J 4 P 1 ( 4) to CMA - J 5 Pl (6) to CMA - J3 Pl (F) to 1st stg - JI Pl (2) to CMA - J7 P 1 ( 3) to CMA - J 1 GRD (f) to EL · grd panel (note 2) GRD (F) togrd rod 1(note3) CMA CMA

Pl ( 1) to CMA · J6 P 1 ( 7 ) to CM A - J 2

From P2 (1) - (note 1) P2 (9) to EL - AlA1J5 P2 ( 13) - (note 1) P2 ( 7) - (note 1) P2 ( 14) - (note 1) P2 (4) ·(note 1) P2 ( 1) - (note 1) P2 (8) - (note 1) GRD (f) to grd rod 1 (note 3) GRD (F) to grd rod 2 (note 3)

To

('

(

(

(

{

(

I

\

·~

Notes: 1. P2 end not connected. Cables, airhose, and conditioned-air duct laid out to facilitate later connection. 2. Connect prior to countdown. 3. Not used in standby, but must be in place to facilitate quick change to firing status.

60W3 60W9 60Wl0 60Wll 60Wl2 60W32 60W34 60W40 60W101 60Wl01 Air duct (note 1) High-pressure airhose (note 1)

Cable

Table 9-5. Preparation for Standby Cabling Data, One Missile

ID

ID

n

Pl (2) to PS· A26J2 Pl (1) to 45 -kw gen. J8 Pl (F) to PS · A26J5 Pl (F) to PS · A26Jl GRD (F) to PTS · A4A4J8 GRD (F) to PTS · A4A4J7 GRD ( F) to EL · grd panel GRD ( F) to grd rod 1 GRD (F) to 45-kw gen· GRD GRD (F) to PDB · Jl2 GRD (F) to grd rod 1 Pl (1) to PDB · J9

From

Notes: 1. Cables installed as part of normal firing position installation. 2. Two ground clamp assemblies are required at this location. 3. Primary usage (standby power). 4. Basic signa l and winterization cables not included.

42W50 (note 1) 58Wl 60Wl6 (note 1) 60Wl7(note1) 60Wl01 (note l) 60Wl01(note1) 60W 101 (note l) 60Wl01 (note 1) 60Wl01 60Wl01 60Wl01 60W l09 (note 3)

Cable

(

P2 (3) to EL· AlAlJl P2 ( 1) to PDB · Jl5 P2 ( 1) to PTS · A4A3J 2 P2 ( 10) to PTS · A4A3J 1 GRD (F) to PS · GRD GRD (F) to EL · grd panel GRD (F) to grd rod 1 GRD ( F) to grd rod 2 GRD (F) to grd rod 1 (note 2) GRD ( F) to grd rod 1 GRD (F) to grd rod 2 P2 (3) to PS· A26J7

To

Table 9-4. Firing Position Auxiliary Power Cabling Data, One Missile

(

I

\

(')

0

'°....

P 1 ( l) to CMA · J 6 Pl (7) to CMA · J2 P l (5) to CMA · J4 Pl (4) to CMA · J5 Pl (6) to CMA · J3 Pl ( F) to 1st stg · J 1 Pl (2) to CMA · J7 Pl (3) toCMA-Jl GRD (f) to EL· grd panel (note 2) GRD (F) to grd rod l (note 3) CMA CMA

From P2 ( 1 ) · ( note 1) P2 (9) to EL · A l A lJ 5 P2 (13) ·( note 1) P2 (7) ·(note 1) P2 ( 14) · (note 1 ) P2 (4) · (note 1) P2( l )·(note 1) P2 (8) ·(note 1 ) GRD (f) to grd rod 1 (note 3) GRD ( F) to grd rod 2 ( note 3)

To

)

Notes: 1. P2 end not connected. Cables, airhose, and condition ed-ai r duct laid out to faci litate later connection. 2. Must be co nnected when changing to fi rin g status. 3. Not used in standby, but must be in place to facil itate quick change to firing status.

60W3 60W9 60Wl0 60Wl 1 60Wl2 60W32 60W34 60W40 60Wl01 60Wl01 Airduct(note 1) H igh -p r essure a irhose ( note 1)

Cable

Table 9-5. Preparation for Standby Cabling Data, One Missile

I

I

.... ....

ID

"""

("')

GRD (F) to grd rod 1 Pl ( 1) to PDB · J 10 Pl (F) to WS blanket · J2 Pl (F) to GS blanket . J l

GOW 101 GOW 109 GOW 114 GOW 11 5

See footnote at end of table .

GRD (F) to EL · grd panel (note 3)

Pl (7) to CMA · J2 Pl (F) to 2nd stg blanket - Jl Pl (F) to 1st stg blanket - Jl Pl (F) to EL · A9J3 GRD (F) to PDB · Jl3

Pl ( l) to 45 -kw gen · JS GRD (F) to PDB · Jl2 GRD (F) to grd rod 1 GRD (F) to 45 -kw gen · GRD

From

GOW 101

Position 2 GOW9 GOW25 GOW25 GOW38 GOW 10 l

58Wl GOWlOl GOW 101 GOW 101

Cable

- J 15 rod 1 ( note 1) rod 2 rod 1

GRD (F) to grd P2 (3) to EL · P2 (F) to EL · P2 ( F) to EL -

rod 2 AlAlJ 1 A8Jl A8J2

P2 (9) to EL· A l AlJ5 P2 ( F) to EL · A9J2 P2 ( F) to EL · A9Jl P2 ( F) to 1st stg · Jl O (note 2) GRD (F) to EL · grd panel GRD ( F) to grd rod 1

P2 ( 1) to PDB GRD (F) to grd GRD (F) to grd GRD (F) to grd

To

Table 9-6. QRA Standby Cabling Data, Two Missiles

I

.c::.

(')

N

...cp

(7) to CMA - J2

GRD (F) to grd rod 1 GRD (F) to EL· grd panel (note 3) P 1 ( 1 ) to PDB - J 11 Pl (F) to WS blanket· J2 Pl ( F) to GS blanket· J 1

(f) to 2nd stg blanket - J 1 (F) to 1st stg blanket - Jl (f) to EL - A9J3 GRD (f) to EL - grd panel GRD ( F) to conductor splice GRD ( f) to conductor splice

Pl Pl Pl Pl

From

(9) to EL· AlA1J5

P2 (3) to EL· AlAlJl P2 (F) to EL - A8Jl P2 (F) to EL - A8J2

GRD (F) to grd rod 2 GRD (f) to grd rod 1

(

{',

{

(

{

{

(F) to EL · A9J2 (F) to EL - A9Jl (F) to 1st stg · J 10 (note 2)

GRD (F) to conductor splice GRD ( f) to conductor splice GRD (F) to PDB · J 14

P2 P2 P2 P2

To

Notes: 1. Two ground clamps required for ground rod 1. 2. Used during standard or confidence count when ambient temperature is - 7°C (20°F) or below, and for 30 minutes prior to starting PS at -32°C (-25°F) or below.

Position 3 60W9 60W25 60W25 60W38 60W101 60W101 60W101 60W101 60Wl01 60Wl09 60Wl 14 60Wl15

Cable

Table 9-6. QRA Standby Cabling Data, Two Missiles-Continued

I

I

~

\

...w

If

~

('")

From

Pl (2) to PS · A26J2 Pl (F} to PS · A26J 5 Pl (F) to PS · A26Jl GRD ( F} to PTS · A4A4J 8 GRD (F} to PTS · A4A4J7

Pl ( 1 ) to 45 -kw gen · JS GRD ( F} to 45 -kw gen· GRD GRD (F) to PDB · J 12 GRD ( F) to grd rod 1

See footnote at end of table .

Position 1 42W50 60Wl6 60Wl 7 60W 101 60W 101

58Wl 60Wl01 60W l 0 1 60W 101

Cable

(

· J 15 rod 1 ( note 1) rod 1 rod 2

P2 (3) to EL . Al AlJl P2 ( 1) to PTS · A4A3J2 P2 ( 10 ) to PTS · A4A3Jl GRD (F} to PS · GRD GRD ( F) to EL . grd panel

P2 ( 1) to PDB GRD ( F) to grd GRD (F) to grd GRD ( F) to grd

To

Table 9-7 . QRA Au xiliary and Stan dby Power Cabling Data, Three Missiles

Notes (Continued): 3. Conn ect prior to countd own .

(

I

-"'

(")

.j:>.

\0

-

GRD (F) toPDB - Jl3 GRD (F) to EL- grd panel (note 3 ) GRD (F) to grd rod 1 Pl(l ) toPDB-JlO

GRD (F) toPDB - Jl4 GRD (F) to conductor spl ice GRD (F) to conductor spl ice GRD (F) to EL - grd pa nel (note 3) GRD (F) to grd rod 1 Pl(l ) toPDB - Jll

Position 2 60W l 01 60W l 01 60Wl01 60W l 09

Position 3 60W l 01 60W l 01 60W 101 60W l 01 60W l 01 60Wl09

Notes: 1. Two ground clamps required for ground rod 1. 2. Bas ic signal and winter ization cab les not included. 3 . Con nect prior to countdown .

GRD (f ) to EL- grd panel (note 3 ) GRD (F) to grd rod 1 Pl (1 ) to PDB- J9

From

60W l 01 60W l 01 60Wl09

Cable

GRD ( F) to conductor splice GRD ( F) to conductor splice GRD (F) to EL - grd panel GRD ( F) to grd rod 1 GRD (F ) to grd rod 2 P2 (3 ) to EL· A l A lJ l

GRD ( F) to EL - grd panel GRD ( F) togrd rod I GRD ( F) to grd rod 2 P2 (3 ) to EL - Al AU 1

GRD (F) to grd rod 1 GRD (F) to grd rod 2 P2 (3 ) to PS - A26J7

To

Table 9-7. QRA Auxiliary and Standby Power Cabling Data, Three Missiles-Continued

I

I

I

'P .... C1'I

~

n

(

(

From

(

P2 ( 1) - (note 1) P2 (9) to EL· AlA1J5 P2 (13) - (note l) P2 (7) - (note 1) P2 (14) - (note 1) P2 ( 1) to PTS · A4A3J2 P2 ( 10) to PTS · A4A3Jl P2 (F) to 10-kw gen - WlJ 1 P2 (F) to EL· A9Jl P2 (f) to EL · A9J2 P2 (4) - (note 1) P2 ( 1) - (note 1) P2 (8) - (note 1) P2 ( 1) to PTS · A4A3J3 P2 (F) to EL - A8J2 (Note 1)

To

Table 9-8. Preparation for Travel Cabling Data

(

Pl (1) to CMA · J6 Pl (7) to CMA - J2 Pl (5) to CMA - J4 Pl (4) to CMA - JS Pl (6) to CMA · J3 Pl (F) to PS· A26J5 Pl (F) to PS - A26Jl Pl (4) to EL· W2Jl P 1 ( F) to 1st stg blanket - J 1 Pl (F) to 2nd stg blanket - J 1 Pl (F) ~o 1st stg - J1 Pl (2) to CMA · J7 Pl (3) to CMA · J1 Pl (F) to vehicle M656 Pl (F) to GS blanket - J1 CMA


60W3 60W9 (note 2) 60Wl0 60Wll 60Wl2 60Wl6 60Wl7 60W2 l (note 3) 60W25 60W25 60W32 60W34 60W40 60Wl08 (note 3) 60W115 Air duct

Cable

{

(

,/

I

"\

....'°.

en

CMA

From

(Note 1)

To

(

{

{

{

(

{

Notes: 1. P2 end not connected. Cables, airhose, and conditioned-air duct bundled and dressed on EL with tiedowns provided. 2. Slack of 60W9 dressed into cable bundle on EL (see note 1 above). 3. Connection for in-transit heating.

High-pressure airhose

Cable

Table 9-8. Preparation for Travel Cabling Data-Continued

~

"\

.... ......

ID

(

Pl (F) to 5-kw gen ( note 2) P 1 ( F) to 5-kw gen (note 3) Pl (7) to GS cntr - J4

60W37 60W37 60W56

P2 ( F) to EH CB - J4 P2 (F) to interconnecting box 10607286 - J3 P2 ( F) to EHCB - J3 or interconn ecting box 10607 286 - J4 (no te 1) P2 ( F) to EHCB - J l P2 ( F) to interconn ecting box 10607286 - J 1 P2 (F) to EHCB - J2

To

Notes: 1. Alternate connection. 2. During in-transit heating, 5-kw generator is mounted on trailer Ml05 , towed by second stage/ guidance section container truck . 3. During in-transit heating, 5-kw generator is mou nted at rear of first stage container truck cargo bed.

Pl (F) to GS cntr - J 14 P l (F) to 1st stg cntr - J l P 1 ( F) to 2nd stg cntr - J 1

From

Table 9-9 . Missile In-Container Heat Cabling Data

(

60W25 60W25 60W25

Cable

(

ID

()

....00

Pl ( F) to GS cn l r · J 14 Pl ( F) lo 5·kw gen - J5 or PDB · J 5 (see note) Pl (7) to GS cn tr - J4

From

Note: Al ternate connection fo r firing site in-con taine r heating.

60W56

60W25 60W37

Cable

P2 ( F) to EHCB - J 2

P2 ( F) lo EHCB · J4 P2 ( F) lo EHCB · Jl

To

Table 9 - 10 . Guidance Section In-Container Heat Cabling Data

I

co

'P ...

n~

{

{

From

(

P2 (1) to 98W3 Pl (1) (note 2)

P2 (3) to EL - AlAlJ 1 P2 (F) to 10-kw gen - J 1 GRD (F) to EL • grd panel GRD ( F) to grd rod 1 GRD ( F) to grd rod 2 P2 (3) to EL - AlAlJ2 P2 (F) to EL • AlAlJ4 Pl (1) to 60W34 P2 (1) (note 2)

To

Table 9-11. EL Electrical Circuit Test Set Cabling Data

(

Pl (2) to PS - A26J2 Pl ( 4) to EL - W2J 1 (see note) GRD (F) to PS· GRD GRD (F) to EL - grd panel GRD ( F) to grd rod 1 P1 ( F) to electrica I circuit test set - J 2 Pl (F) to electrical circuit test set - J 1 Red to electrical circuit test set - DC + Black to electrical circuit test set - DC Pl (2) to CMA · J7

{

Notes: 1. Alternate generator connection. 2. Installation for cable mast and clamp release mechanism test.

60W34

42W50 60W21 60Wl01 60Wl01 60W101 98Wl 98W2 98W3

Cable

(

~

I

\

flt .OU;

.------ - - -

.~!...----1-=---"J;ifl-"""''-i~.

'1 I I \ j-------~.i71.!!~~J...!'-L--~-"{7f}---='---{~A

I

.,.,..,,,

I

\

t--------~~a-~~+-"''-~avi

I

I

\

L------I

Ill"''-~--+-=-~-"'~

I

I

~------- - vrz.---r''-----"'V1J-"""I

I I

..

\

~-------.171!!~~-t2:!--,-'~)-~-{7[~

,,,,, "'"'''

I I

I

r--- --- --~·l7feL,--i-"'-r'-'V'I I

i

\

~-------ITTl!!L..f~-+-"---t~~ll:I----"=-(~

I I

I :

~'~~

::-"'""

'::fff"~

~CIM

L----------------------~ #OflS I

,_,AIN,ltJ, T{JflNdNOl,Jt ftD.

I

/MM"IOllld/Ntjl(,t1/$ (AdU.S AlTIJf-111,. "'4Nt
I

Figure 9 - 1. Cable mast cable test connections.

9-20

Cl

N

'°...

Pl ( 1) to 45·kw gen - JS Pl ( 1) to PDB - J9 P l (1) to PDB · JlO P 1 ( 1 ) to PDB - J 11 GRD (F ) to 45 -kw gen - GRD GRD (F ) to PDB - Jl2 GRD ( F) to grd rod 1

From

To

P2 ( 1) to PDB - J 15 P2 (2) to RTS - J15 P 2 ( 2) to RTS - J 1 5 P2 (2) to RTS - J 15 GRD (F) to PDB - Jl 3 GRD (F) to grd rod 1 GRD (F) to grd rod 2

Note: 58W 1 is a multiusage cable from motor generator cable reel s.

58W 1 (see note) 60W20 60W20 60W20 60W l 01 60W 101 60W 101

Cable

Table 9-12. Headquarters Battery Cabling Data

l

n

~

'°~

Pl ( 2) to FDT - A2JS P 1 ( 1) to FDT - A2J 7 Pl (F) to FDT - A2J2 Pl (F) to FDT - A2J6 Pl (1) to 45-kw gen - JS Pl (1) to 45-kw gen - JS GRD (F) to 45-kw gen - GRD GRD (F) to FDT · GRD GRD (F) to 45-kw gen · GRD GRD (F) to SCTS · A32A4A4J7 GRD (F) to grd rod 1 Pl (F) to FDT · A2J3 Headset (F) Headset (F) Headset ( F)

From

{

{

{

To

(

{·

(

P2 (3) to SCTS - input pwr J3 P2 ( 1) to SCTS · input pwr J2 P2 (10) to SCTS - A32A4A3Jl P2 ( 1) to SCTS - A32A4A3J2 P2 ( 1) to FDT - A2J4 P2 ( 1) to FDT - A2J 5 GRD (F) to SCTS - A32A4A4J 10 GRD (F) to SCTS - A32A4A4Jl 1 GRD (F) to SCTS · A32A4A4J9 GRD (F) to grd rod 1 GRD (F) to grd rod 2 P2 ( 2) to input pwr J 1 SCTS - A32A4A4J 1 SCTS - A32A4A4J2 FDT - A2J16

Note: 58Wl is a multiusage cable from motor generator cable reels.

42W50 43W6 43W9 43Wl0 58Wl (see note) 58Wl (see note) 60Wl01 60Wl01 60Wl01 60Wl01 60Wl01 60Wl 10

Cable

Table 9-13. SCTS Cabling Data, Using PSE

I

~

'

w

N

IO

.

-n

28W3 28W5 28W6 28W8 28W9 28W l 0 60W3 60W9 60W 10 60Wl l 60Wl2 60W l 6 60Wl 7 60W32 60W34 60W40 60W l 0 1 5 0W 10 l 60W 10 1 60W 101

Cable

(

Fro m

To P2 ( 1) to GS cntr · Wl3J 13 P2 ( 1) to GS cntr. WllJ l l P2 (6) to GS cntr · WlOJ 10 P2 (2) to 2nd stg cntr. W7J 7 P2 ( 5) to 2 nd stg cntr · W6J6 P2 ( 1) to 2nd stg cntr · W5J 5 P2 ( l ) to PS · A26J 6 P2 (9) to PTS · A4A 1J 8 P2 ( 13) to PTS · A4A lJ4 P2 (7) to PTS · A4A1J 5 P2 ( 14) to PTS · A4A 1J3 P2 ( 1) to PTS · A4A3J2 P2 ( 10) to PTS · A4A3J 1 P2 (4) to PTS · A4AlJ9 P2 ( 1) to PTS · A4A1J7 P2 (8) to PTS - A4AlJ6 GRD ( F) to PTS - A4A4 J 1 1 GRD ( F) to PTS · A4A4J8 GRD (F} to grd rod 1 GRD (F) to grd rod 2

Table 9 -14. Missile In-Container Test Cabling Data

(

P 1 ( 1) to 2nd stg en tr . W 1J1 Pl ( 1) to 2nd stg cntr · W3J3 P l (12) to 2nd stg cntr · W2J2 Pl (1) to 1st stg cntr · W3 J 3 P l (1 1) to 1st stg cntr · W2 J 2 P l (1) to 1st stg cn tr. Wl J l P l ( 1) to GS cntr · W9J9 P l (7) to GS cntr. W4 J4 Pl (5) to GS cntr · W7J7 P 1 ( 4) to GS cntr - W8J 8 Pl (6) to GS cntr - W5J5 Pl (F) to PS· A26J5 Pl ( F) to PS. A26Jl P l (F) to ls! stg cntr · W5J5 Pl (2) to GS cntr - W6J6 Pl (3) to GS cntr. W3J3 GRD (F} to PS· GRD GRD (F} to 1st stg cn l r - GRD GRD ( F} to PTS · A4A4J 7 GRD ( F) to grd rod 1

(

I

I

IO

U'I

!>)

GRD (F) to PTS · A4A4J8 Pl (1) to 1st stg cntr · WlJl Head set ( F) Headset (F)

60W101 60W 111

GRD (F) to PTS · A4A4J11 GRD ( F) to grd rod 1 GRD ( F) to grd rod 2 or 1st stg · GRD (see note) GRD (F) to 1st stg cntr · GRD P2 ( 1) to PS · A26J 6 PTS · A4A4Jl PS· A26J4

To

(

Note: When fir st stage is un der maintenance, disconnect 60W101 from ground rod 2 and connect to ground on first stage. Disconnect all cab les from container.

GRD (F) to PS· GRD GRD (F) to PTS · A4A4J7 GRD (F) to grd rod 1

From

Table 9 - 15. First Stage In-Container Test Cabling Data-Continued

(

60W l 01 60Wl01 60Wl01

Cable

c

)

n

°'

'°N

Pl (1) to 2nd stgcntr - WlJl Headset (F) Headset (F)

60W112

P2 (6) to PTS - A4A2J8 P2 (2) to PTS · A4A2J 5 P2 (2) to 2nd stg cntr - W7J7 P2 (5) to 2nd stg cntr - W6J6 P2 (1) to 2nd stg cntr · W5J5 P2 ( F) to PTS - A4A4J8 P2 ( 1) to PTS · A4A3J2 P2 ( 10) to PTS - A4A3J 1 GRD (F) to PTS · A4A4J 11 GRD (F) to grd rod 1 GRD (F) to grd rod 2 or 2nd stage - GRD (see note) P2 (1) to PS - A26J6 PTS - A4A4Jl PS· A26J4

To

(

(

(

{·

(1

f.

Note: When second stage is under maintenance, disconnect 60Wl01 from ground rod 2 and connect to ground on second stage. Disconnect all cables from container.

Pl (12) to 2nd stgcntr - W2J2 Pl ( 1) to 2nd stg cntr - W3J3 Pl (1) to PTS -A4A2J4 Pl ( 11) to PTS - A4A2J6 Pl ( 1) to PTS - A4A2J2 Pl (f) to PTS - A4A4J6 Pl (F) to PS - A26J5 Pl (F) to PS· A26J 1 GRD (F) to PS· GRD GRD (F) to PTS · A4A4J7 GRD (F) to grd rod 1

From

28W6 28W8 28W8 28W9 28Wl0 32Wl0 60Wl6 60Wl7 60Wl01 60Wl01 60Wl01

Cable

Table 9-16. Second Stage In-Container Test Cabling Data

~

I

I

I

'\

~ .....

ID

n

28W3 28W5 28W6 32Wl0 60W3 60W9 60Wl0 60Wl l 60Wl2 60Wl6 60Wl7 60W34 60W40 60Wl01 60Wl01 60Wl01

Cable

c

I

(

P 1 ( 1) to PTS · A4A2J 3 Pl (1) to PTS · A4A2J4 Pl (12) to PTS · A4A2 J7 Pl (1) to PTS · A4A4J6 Pl (1) to GS cntr · W9J9 Pl (7) to GS cntr · W4J4 Pl (5) to GS cntr · W7J7 Pl (4) to GS cntr · W8J8 Pl (6) to GS cntr · W5J5 Pl (F) to PS· A26J5 P 1 ( F) to PS · A26J 1 Pl (2) to GS cntr · W6J6 Pl (3) to GS cntr · W3J3 GRD (F) to PS· GRD GRD (F) to PTS · A4A4J7 GRD (F) to grd rod 1 Headset ( F) Headset (F) Dummy connector 32A4AlP6

From P2 ( 1) to GS cntr · Wl3Jl3 P2 ( 1) to GS cntr · WllJll P2 (6) to GS cntr · WlOJlO P2 (F) to PTS · A4A4J8 P2 ( 1) to PS · A26J6 P2 (9) to PTS · A4AlJ8 P2 ( 13) to PTS - A4A1J4 P2 (7) to PTS · A4A1J5 P2 ( 14) to PTS · A4AlJ3 P2 ( 1) to PTS · A4A3J2 P2 ( 10) to PTS · A4A3J 1 P2 (1) to PTS · A4AlJ7 P2 (8) to PTS · A4A1J6 GRD (F) to PTS · A4A4Jll GRD ( F) to grd rod 1 GRD (F) to grd rod 2 PS · A26J4 PTS · A4A4Jl GS cntr · WlJ 1

To

-

Table 9-17. Guidance Section In-Container Test Cabling Data

(

I

)

'P

N

n

CD

(

Pl Pl P1 P1 Pl Pl

(

From

GS cntr GS cntr

To

(F) (2) ( 1) ( F) (F) ( 1)

to to to to to to

{

SCTS · A32A4A4J6 FDT · A2J8 FDT · A2J 7 FDT · A2J 2 FDT- A2J6 45-kw gen ·JS

From P2 P2 P2 P2 P2 P2

(

{1

(f) to SCTS · A32A4A4J8 (3) to SCTS · input pwr J3 ( 1) to SCTS · input pwr J 2 ( 10) to SCTS · A32A4A3J 1 (1) to SCTS • A32A4A3J2 (1) to FDT • A2J4

To

Table 9-18. Azimuth Laying Control Box Test Cabling Data

PS PS


32Wl0 42W50 43W6 43W9 43Wl0 58Wl (see note)

Cable

Air duct High-pressure airhose

Cable

{,

Table 9-17. Guidance Section In-Container Test Cabling Data-Continued

~

m

\

'°N '°

n

{

(

{

{

(

To P2 ( 1) to FDT · A2J 5 P2 (15) to SCTS · A32A4A1J2 GRD (F) to SCTS · A32A4A4J 11 GRD (F) to SCTS · A32A4A4J 10 GRD (f) to SCTS · A32A4A4J9 GRD (F) to grd rod 1 GRD (F) to grd rod 2 P2 (2) to SCTS · input pwr Jl FDT • A2J 16 SCTS • A32A4A4J 1 SCTS · A32A4A4J2 ALCB · J6


Pl (1) to 45-kw gen - JS Pl (F) to ALCB · Jl GRD (F) to FDT · GRD GRD (F) to 45-kw gen - GRD GRD (F) to 45-kw gen · GRD GRD (F) to SCTS • A32A4A4J7 GRD (F) to grd rod 1 Pl (F) to FDT · A2J 3 Headset (F) Headset (F) Headset (F) Headset (F)

From

Table 9-18. Azimuth Laying Control Box Test Cabling Data-Continued

SSW 1 (see note) 60W44 60Wl01 60Wl01 60Wl01 60Wl01 60Wl01 60W110

Cable

(

~

I

'

ID

...w

FDT

FDT FDT

Pl (2) to GS cntr · W6J6 Pl (3) to GS cntr · W3J3 GRD (F) to 1st stg cntr · W6J6 GRD (F) to FDT · GRD GRD (F) to 45-kw gen· GRD GRD (F) to 45-kw gen· GRD GRD (F) to SCTS · A32A4A4J7 GRD ( F) to grd rod 1 Dummy connector 32A4AlP6 Headset (F) Headset (F) Head set ( F) Pl (F) to FDT · A2J3

From

To P2 (1) to SCTS · A32A4AlJ7 P2 (8) to SCTS · A32A4AlJ6 GRD (F) to SCTS · A32A4A4J8 GRD (F) to SCTS · A32A4A4Jll GRD ( F) to SCTS · A32A4A4J 10 GRD (F) to SCTS · A32A4A4J9 GRD (F) to grd rod 1 GRD ( F) to grd rod 2 GS cntr · WlJl FDT · A2Jl6 SCTS · A32A4A4J 1 SCTS · A32A4A4J2 P2 (2) to SCTS · input pwr Jl GS cntr GS cntr GS cntr


60W l 10 Air duct Air du ct High-pressure airhose

60W34 60W40 60Wl01 60Wl01 60Wl01 6 0W l01 60Wl01 60Wl01

Cable

Table 9-19. Missile In-Container Test Cabling Data, Using PSE-Continued

{

")

n

-

N

'°w

{

From

{

(•

Pl (1) to 1st stg cntr • W3J3 Pl ( 11) to 1st stg cntr • W2J2 Pl (2) to FDT • A2JS P 1 (1 ) to FDT · A2J 7 Pl (F) to FDT · A2J 2 Pl (F) to FOT · A2J6 Pl ( 1) to 45-kw gen ·JS Pl (1) to 45-kw gen· JS Pl (F) to 1st stg cntr · W5J5 GRD (F) to 45-kw gen · GRD GRD (F) to 45-kw gen· GRD GRD (F) to 1st stg cntr · GRD GRD (F) to SCTS · A32A4A4J7 GRD (f) to grd rod 1 GRD (f) to SCTS • A32A4A4J 11 Pl (F) to FOT · A2J 3


2SWS 2SW9 42W50 43W6 43W9 43W10 5SW 1 (note 1) 5SW 1 (note 1) 60W32 60Wl01 60Wl01 60Wl01 60Wl01 60Wl01 60Wl01 60Wl 10

Cable

{

()

{,

P2 (2) to SCTS · A32A4A2J5 P2 ( 5) to SCTS · A32A4A2Jl P2 (3) to SCTS · input pwr J3 P2 (1) to SCTS · input pwr J2 P2 ( 10) to SCTS · A32A4A3J 1 P2 ( 1) to SCTS • A32A4A3J 2 P2 ( 1) to FDT • A2J4 P2 ( 1) to FDT · A2J 5 P2 (4) to SCTS · A32A4A1J9 SCTS · A3 2A4A4J 10 SCTS · A32A4A4J9 GRD (F) to SCTS · A32A4A4JS GRD (F) to grd rod 1 GRD (f) to grd rod 2 or 1st stg (note 2) GRD (f) to FDT · GRD P2 ( 2) to SCTS · input pwr J 1

To

Table 9-20. First Stage In-Container Test Cabling Data, Using PSE

I

I

/

\

w w

IO

Pl ( 1) to 1st stg cntr - WlJl Headset (F) Headset (F} Headset ( F)

From P2 ( 1) to FDT - A2J 1 FDT - A2J 16 SCTS - A32A4A4J 1 SCTS - A32A4A4J 2

To

Notes: L 58Wl is a multiusage cable from motor generator cabl e r eels. 2. When f irst stage is to undergo maintenance, disconnect 60Wl01 from ground rod 2 and connect to GRD on first stage.

60W 111

Cabl e

Table 9-20. First Stage In-Container Test Cabling Data, Using PSE- Continued

(

')

n

-

~

'°w

{

From

{

{

Pl (12) to 2nd stg cntr · W2J2 Pl (l) to 2nd stg cntr · W3J3 Pl (1) to SCTS · A32A4A2J4 Pl ( 11) to SCTS · A32A4A2J6 Pl ( 1) to SCTS · A32A4A2J2 Pl (F) to SCTS · A32A4A4J6 Pl (2) to FDT · A2J8 P 1 ( 1 ) to FDT · A2J 7 Pl (F) to FDT · A2J2 Pl (F) to FDT · A2J6 Pl ( 1) to 45-kw gen ·JS Pl ( 1) to 45-kw gen· J8 GRD ( F) to FDT · GRD GRD (F) to 45-kw gen · GRD GRD (f) to 45-kw gen · GRD GRD ( F) to SCTS • A32A4A4J 7


28W6 28W8 28W8 28W9 28Wl0 32Wl0 42W50 43W6 43W9 43Wl0 58Wl (note 1) 58Wl (note 1) 60Wl01 60Wl01 60Wl01 60Wl01

Cable

{

{I

{I

P2 (6) to SCTS · A32A4A2J8 P2 (2) to SCTS · A32A4A2J5 P2 (2) to 2nd stg cntr • W7J7 P2(5)to2nd stg cntr · W6J6 P2 (1) to 2nd stg cntr · W5J 5 P2 (F) to SCTS · A32A4A4J8 P2 (3) to SCTS · input power J3 P2 ( 1) to SCTS · input pwr J2 P2 ( 10) to SCTS · A32A4A3J 1 P2 ( 1) to SCTS · A32A4A3J 2 P2 ( 1) to FDT · A2J4 P2 ( 1) to FDT · A2J 5 GRD ( F) to SCTS · A3 2A4A4J 11 GRD (F) to SCTS · A32A4A4J9 GRD (F) to SCTS · A32A4A4Jl0 GRD (F) to grd rod 1

To

Table 9-21. Second Stage In-Container Test Cabling Data, Using PSE

I

I

I

~

\

U1

w

ID

( (

GRD ( F) to grd rod 1 Head set ( F) Headset ( F) Headset (F) Pl (F) to FDT · A2J3 Pl (1) to 2nd stg cntr - WlJl

From

GRD ( F) to grd rod 2 or 2nd stg ( note 2) FDT - A2J 16 SCTS - A32A4A4J 1 SCTS - A3 2A4A4J2 P2 ( 2) to SCTS - input pwr J 1 P2 ( 1) to FDT - A2J 1

To

Notes: 1. 58W 1 is a multiusage cable from motor generator cabl e reels. 2. When second stage is to undergo maintenance, disconnect 60W l0 1 from ground rod 2 and connect to ground on second stage.

60Wl 10 60Wl 12

60Wl01

Cable

Table 9-21. Second Stage In-Container Test Cabling Data, Using PSE-Continued

(

ID

n

al

w

See footnote at end of tabl e.

(1) to SCTS · A32A4A2J3 (1) to SCTS · A32A4A2J4 ( 12 ) to SCTS · A32A4A2Ji (F) to SCTS · A32A4A4J6 (2) to FDT · A2J8 ( l) to FDT · A2J7 (F) to FDT · A2J2 (F) to FDT · A2J6 (1) to 45-kw gen. J8 ( 1) to 45-kw gen. J8 (1) to GS cntr · W9J9 (7) to GS cntr · W4J4 (5) to GS cntr. W7J7 (4) to GS cnt r . W8J8 (6) to GS cn tr . W5J5 (2) to GS cntr · W6J6 (3) to GS cntr · W3J3

28W3 28W5 28W6 32W10 42W50 43W6 43W9 43Wl0 58W 1 (see note) 58W 1 (see note) 60W3 60W9 60Wl0 60Wl 1 60Wl2 60W34 60W40

Pl Pl Pl Pl Pl Pl Pl Pl Pl Pl Pl Pl Pl Pl Pl Pl Pl

From

Cable P2 P2 P2 P2 P2 P2 P2 P2 P2 P2 P2 P2 P2 P2 P2 P2 P2

(1) to GS cntr · Wl3Jl3 (1) to GS cntr · WllJll (6) to GS cntr · WlOJ 10 (F) to SCTS · A32A4A4J8 (3) to SCTS · input pwr J3 ( 1) to SCTS · input pwr J2 ( 10) to SCTS · A32A4A3J 1 ( 1) to SCTS · A32A4A3J 2 ( 1 ) to FDT · A2J4 ( 1 ) to FDT · A2J5 ( 1 ) to FDT · A2J 1 (9) to SCTS · A32A4AlJ8 ( 13) to SCTS · A32A4A1J4 (7) to SCTS · A32A4A 1J5 ( 14) to SCTS · A32A4A 1J 3 ( 1) to SCTS · A32A4Al J 7 (8) to SCTS · A32A4A1J6

To

Table 9- 22. Guidance Section In-Container Test Cabling Data, Using PSE

I

I

I

IO

' w ....,

To GRD (F) to·SCTS · A32A4A4Jll GRD (F) to SCTS · A32A4A4Jl0 GRD (F) to SCTS · A32A4A4J9 GRD (F) to grd rod 1 GRD (F) to grd rod 2 P2 (2) to SCTS - input pwr J 1 GS cntr - W lJ 1 FDT · A2J 16 SCTS - A32A4A4J 1 SCTS - A32A4A4J2 GS cntr GS cntr GS cntr

From

GRD (F) to FDT · GND GRD ( F) to 45 -kw gen· GRD GRD ( F) to 4 5-kw gen · GRD GRD (F) to SCTS - A32A4A4J 7 GRD (F) to grd rod 1 Pl(F) to FDT - A2J3 Dummy connector 32A4AlP6 Headset ( F) Headset (F) Headset (F) FDT ·FDT FDT

Note: 58W 1 is a mu ltiusage cable from motor generator cable reels.

Air duct Air d uct High-pressure airhose

60Wl01 60Wl01 60Wl01 60Wl01 60W l01 60W110

Cable

Table 9-22 . Guidance Section In-Container Test Cabling Data, Using PSE-Continued

(

')

00

'°w

(l

Air inlet High-p ressu re airhose

32Wl0 42Wl 42W2 42W3 42W4 42W5 42W6 42W7 42W8 42W9 42Wl0 42Wl8 60Wl01 60Wl01

Cable

{

(;

Pl to SCTS - A32A4A4J6 Pl to SCTS pneu test console - J56 Pl to SCTS pneu test console - J57 Pl to SCTS pneu test console - J58 Pl to SCTS pneu test console - J59 Pl to SCTS pneu test console - J60 Pl to SCTS pneu test console - J62 Pl to SCTS pneu test console - J61 Pl to SCTS pneu test console - J63 Pl to SCTS pneu test console - J64 Pl to SCTS pneu test console - J65 Pl to SCTS pneu test console - J 135 GRD (F) to SCTS - A32A4A4J7 GRD (F) to grd rod 1 Dummy connector 11035469 GS blower SCTS pneu test console

From

(

(

P2 to SCTS - A32A4A4J8 P2 to GS - WlJl P2 to GS - W2J2 P2 to GS - W3J3 P2 to GS - W4J4 P2 to GS - W5J5 P4 to GS - W6J6 P2 to GS - W7J7 P2 to GS - Wl9J3 P2 to GS - W20J2 P2 to GS - W24J2 P2 to GS blower GRD (F) to grd rod 1 GRD (F) to grd rod 2 GS- 7WlP2 GS GS

To

Table 9-23. Guidance Section In-Van Cabling Data

(

~

\

IO

w

IO

PNEUMATIC TE.ST CON50lE CONNECTOR PANEl 9SA2A2

9SA2"3

PRE55URE TE.ST .$ET

(

J(,0

Jt.2

/NO/CATES MAU ("ONNECTOR.

-li!W5

42Wt.

1057~4(,8

N/GN•PNE55UR£ AIRN05£

NIGN· PN£5SllRE A IN NO.SE /10.179$5

(

I

I I

I

I

I I I

I

WS./5

FSNB· ~B

I I I _ _ _ _ _ _ _ _ _J Wt../&.

- ----

UMS/l/CA£ ("ONNECTIONS

CUIOANCE .$£CT/ON 8 (/N TE.57 OOllY)

Figure 9-2. Guidance section pressure test.

0

NOT~:

Pl

Pl

COMPT: A/R SUPPlY

COMPT: PRE55. CHECK

(

0

'°,i.

{\

.151

D

(r

IZl

Pl

1051"4'~~"

AIRHOSE

Nlt:H·PRESStlRE

./2W2

DOOR

BATTERY ACCESS

P2

I

{.:

l

uiiB1Licii coNA.iecnoZl

"

l

TO.AIR

WPUT FILTER

I

iI

---i1

BOTTLE

{

{

L - - - - - - - ____ .....J

SWITCH

P!?C~JllRE

r7;;Pllrc"RO"ss

A IllHOSE 11027461

-----------'

WU2

Figure 9-3. Pressure switch test setup.

INDICATES MAI.£ CONNEroR.

NOTE:

Hl&H-PRE.SStlHE AIR CdtPLIA/$

'5A2

PNEUMATIC TEST CONSQi.£ CONNECTOR PANEi.

&ii/DANCE SCCTION 8 (IN TE.ST 001.l.Y)

TO

(

FSNB·f5

UMBILICAi.

~

\

6(.1/0ANCC SEcrtON tJ

(IN TEST POLLY) ~ESivJie

PNEUMATIC

- - --,

TESTCQV~E

C-QNNECTOR

PANEL 95;12

Pt

PZ 4ZN9

~:ECTION

4ZWZ

I I I I

42Wt;

:::~::~~~'::£~===H==l~=H=·=P,=~=ES.=SV. ==~=E===t=1 All?HOSE 1057<:>4611

I I -l

____ _ J

PNEllM.4TIC TEST !15A2.42

CH.45515

-

NOT£

12'.'.J 1NPIC.4rl'S M.4LE C
TOST-120 FSN8·f6

Figure 9-4. Air pressure test setup.

9-41

1r---1' --

r-----1

::()~~: ~~I ~ 11

1I

11 11 i

li:1

1 I~

11!?.___

9.42

-,

II

~

~~II

.! I : I

_ _ _ _ __J

I

Table 9-24. Connector Pin Number-to-Letter Cross-Reference No.

Letter

No.

Letter

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21

A B

22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41

y

c

D

E

F

G

H

J

K

L M

N

p

R

s

T

u

v w x

z

a

b

c

d e f g h

i

km n p

q

r ~

t

No.

Letter

42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61

.Y ~

w ~

y

z

AA BB

cc

DD

EE

FF

GG

HH JJ

KK

LL

MM

NN

pp

Table 9-25. Cable Transport or Storage Area Data Item

Transport or storage area Firing Position Power Distribution Set

42W50 42W54 60W3 'W 60W9

60Wl0

Coiled in vehicle Coiled in vehicle In bundle In bundle In bundle

forward cargo area of PTS/PS forward cargo area of PTS/PS on EL on EL on EL

9.43

Table 9-25. Cable Transport or Storage Area Data- Continued Item

Tran sport or storage area

Firing Position Power Distribution Set-Continued 60Wl 1 60Wl2 60W16 60Wl7 60W21 60W25 60W32 60W34 60W38 60W40 60W43 60W44 60Wl01 60Wl03 60Wl05 60W l09 60Wl 14

60W 115

I

Conditioned air duct High -press ure airhose Ground rod Groun d clamp Power distribution box Cable reel assembly

9-44

In bund le on EL In bundle on EL Connected between PTS and PS on PTS / PS ve hicle Connected between PTS and PS on PTS / PS vehicle Connected from tractor XM 7 5 7 to EL for missile transit; stored on XM7 57 Coiled on auxiliary eq uipmen t vehicle; winterized operation . operating posi· tion on EL In bundle on EL In bundle on EL Coi led on auxiliary equipment vehicle In bun dle on EL On aux iliary equipment vehicle On auxi liary equipment vehicle Four co iled in forward cargo area of PTS / PS vehicle; three coi led onauxilia ry equipment ve hicle Coiled in forward cargo area of PTS/PS vehic le On reel stowed on auxiliary equipment vehicle On auxiliary equi pment vehicle Normal ope ration · coiled on auxiliary equipment vehicle; winterized operation · connected to warhead section blanket on EL Normal operation · connected to gu id· a nee section blanket on EL In bundle on EL In bundle on EL Auxiliary equipment vehicle Auxiliary equipment veh icle Auxiliary equipment vehicle Auxiliary equip ment vehicle

C2

Table 9-25. Cable Transport or Storage Area Data-Continued Item

Transport or storage area

EL/ Missile Auxiliary Power Distribution Set

60W3 60W9 60W10 60Wll 60W12 60W21 60W25 60W32 60W34 60W38 60W40 60W101 60Wl09 60W114

60W115 High pressure airhose Conditionedair duct Ground clamp Ground rod Conductor splice

In bundle on EL In bundle on EL In bundle on EL In bundle on EL In bundle on EL Connected from tractor XM757 to EL for missile transit; stored on XM757 Coiled on auxiliary equipment vehicle; winterized operation · operating position on EL In bundle on EL In bundle on EL Coiled: on auxiliary equipment vehicle In bundle on EL Four coiled on auxiliary equipment vehicle On auxiliary equipment vehicle Normal operation ·coiled in auxiliary equipment vehicle; winterized operation • connected to warhead section blanket on EL Normal operation · connected to guidance section blanket on EL In bundle on EL In bundle on EL Auxiliary equipment vehicle Auxiliary equipment vehicle Auxiliary equipment vehicle

Forward Area Test Cable Set

28W3 28W5 28W6

C2

Coiled in battery Coiled in battery Coiled in battery

front of parts shelter on firing maintenance vehicle front of parts shelter on firing maintenance vehicle front of parts shelter on firing maintenance vehicle

9.45

I

Table 9-25. Cable Transport or Storage Area Data-Continued Transport or storage area

Item

Forward Area Test Cable Set-Continued 28W8

Coiled in front of parts shelter battery maintenance vehicle Coiled in front of parts shelter battery maintenance vehicle Coiled in front of parts shelter battery maintenance vehicle Coiled in front of parts shelter battery maintenance vehicle Coiled in front of parts shelter battery maintenance vehicle Coiled in front of parts shelter battery maintenance vehicle

28W9 28W10 60Wl01 60Wlll 60W112

on firing on firing

'-"

on firing on firing on firing

.._,,.

on firing

Guidance Section In-Container Heat Set 60W25 60W37 60W56 Electrical heating con· trol box

Connected on guidance section container truck Connected on guidance section container truck Connected on guidance section container truck Guidance section container truck

Missile In-Container Heat Set 60W25 60W37 60W56

9-46

In connected position: two on second stage/guidance section container truck; one on first stage container truck In connected position: one each on first stage container truck and second stage/ guidance section container truck In connected position: on second stage/ guidance section container truck

'9.1

'9.1


Transport or storage area Missile In-Container Heat Set-Continued

Electrica I heating control box Interconnecting box

On second stage/ guidance section con· tainer truck On first stage container truck

Headquarters Battery Cable Set 60W20 60Wl01 Power distri· bution box Ground rod Ground clamp assembly

On AN / TRC-80 transport truck M656 On 45-kw generator towing vehicle On 4 5-kw generator towing vehicle On 45-kw generator towing vehicle On 45 -kw generator towing vehicle

Direct Support Cable Set 28W3 28W5 28W6 28W8 28W9 28Wl0 42W50 43W6 43W9 43Wl0 60W3 60W9 60Wl0 60Wl 1 60Wl2 60W32 60W34

Cable 1, reel Cable 2, reel Cable 3, reel Cables 1 and trailer Cable 3, reel Cable 4, reel Cable l, reel on cable reel Cable 1, reel Cable 2, reel Cable 2, reel Cable 1, reel Cable 3, reel Cable 1, reel Cable 2, reel Cab le 3, reel Cable 1, reel Cable 2, reel

on on on reel

cable reel trailer cable reel trailer cable reel trailer 2, on cable reel

2, on 2, on 8, and trailer 7, on 7, on 8, on 4, on 7, on 6, on 6, on 6, on 3, on 3, on

cab le reel trailer cable reel trailer cable 3, reel 4,

1, 1, l, 2,

cable cable cable cable cable cable cab le cab le cable cable

reel reel reel reel reel reel reel reel r eel reel

trailer trailer trailer trailer trailer trailer trailer trailer trailer trailer

9-47


Transport or storage area Direct Support Cable Set-Continued

60W40 60W44 60Wl01

I

60Wl 10 60Wl 11 60W l l 2 Ground clamp Ground rod s

I

Cabl e 3, reel 3, on Cable 2, reel 4, on Cables 1 th ru 7, on trailer Cable 3, r eel 8, on Cable 1, reel 5, on Cable 2, r eel 5, on On ca ble reel trailer On ca ble reel trailer

cable reel trailer cable reel trailer reel 9, cab le reel cable reel trailer cable reel trailer cable reel trailer

Other Interconnecting and Test Cables

22A35W l 22A35W2 22A35W3 22A35W4 22A35W5 22A35W6 22A35W7 22A35W8 25Wl 25W3 25W4 25W5 25W6 25W7 25W8 25W9 25Wl0 25Wl 1 25Wl3 25Wl4 26Wl 26W2 26W3 26W5 26W6 26W7 26W9

9-48

Part of ca ble mast assembly Part of cable mast assembly Part of cable mast assembly Part of cable mast assembly Part of cable ma st assembly Part of cable mast assembly Part of cable mast assembly Part of cable mast assembly Part of guidan ce section container Part of guidance section conta in er Part of guidan ce section container Part of guidance section container Part of guida nce section container Part of guidance section container Part of guidance section container Part of guidan ce section container Part of guida nce section container Pa rt of guidance section container Part of guidance section contai ner Part of guidance section contai ner Pa rt of second stage container Part of secon d stage con tainer Pa rt of secon d stage container Part of second sta ge con tain er Part of second stage container Pa rt of second sta ge container Pa rt of second sta ge container

Cl

Table 9-25. Cable Transport or Storage Area Data- Continued Item

Transport or storage area

Other Interconnecting and Test Cables - Continued 27Wl 27W2 27W3 27W5 27W6 32W10 42Wl 42W2 42W3 42W4 42W5 42W6 42W7 42W8 42W9 42W10 42W13 42Wl4 58Wl 60W l 8 60W108 69Wl 69W3 76W3 98Wl 98W2 98W3

Cl

Part of first stage container Part of first stage container Part of first stage container Part of first stage container Part of first stage conta iner In PTS storage cabinet Forward sto rage area of SCTS Forward storage area of SCTS Forwa rd stor age a r ea of SCTS Forward storage area of SCTS Forward storage area of SCTS Forward storage area of SCTS Fo rward storage area of SCTS Forward storage area of SCTS Forward storage a rea of SCTS Forward .storage area of SCTS Forward storage area of SCTS Forward storage area of SCTS On reel on motor generator trailer On reel in PTS Connected between PTS and vehicle power system on PTS / PS vehicle Shop sets Mechanica l shop set In firing position tool kit carried on auxiliary equipment vehicle On auxiliary equipment vehicle On auxiliary equipmen t vehicle On auxi liary equipment vehicle

9-49

I

Table 9-26. RFI Cables Reference designation

42W54 60W9 60W10 60Wll 60W12 60W18 60W32 60W34 60W40 60W44 60W105

9·50

Reference No.

11039299-9 11039300-9 11039301-9 11039302-9 11039303-9 11039304-9 11039305-9 11039306-9 11039307-9 11039308-9 11039221-49

C4

'°Ui

-

~

(")

Cable

{


22A35Wl 22A35W2 22A35W3 22A35W4 22A35W5 22A35W6 22A35W7 22A35W8 25Wl 25W3 25W4 25W5 25W6 25W7 25W8 25W9 25W10

(

I

{

11039314 11039310 11039313 11039311 11039312 10574079 11039315 11039316 10625175 10625176 10625177 10625178 10625179 10625180 10625181 10625182 11025978

Reference No.

17.58 17.75 17.25 17.25 17.0 18.0 21.67 18.17 5.0 10.6 13.0 11.25 14.0 13.7 11.7 13.4 9.4

Length (ft.)

Table 9-27. Cable Data

{

(

60 60 60 60 60 6 (branched)' 60 (branched)' 16 60 60 60 60 60 60 60 6 60

Number of conductors

(

~

I

~

~

0

N

'°u..

(,

{r


25Wll 25W13 25W14 26Wl 26W2 26W3 26W5 26W6 26W7 26W9 27Wl 27W2 27W3 27W5 27W6 28W3 28W5

Cable

(1

11025566 10625186 10574740 10625187 11025979 11025568 11026164 11026165 11026166 10645840 11026167 11026168 11026169 10625199 10578255 11039273 11039274

Reference No.

(

9.7 9.8 9.2 15.8 16.7 17.9 12.0 12.0 12.0 3.33 16.0 14.6 16.0 12.25 13.0 25 25

Length (ft.)

Table 9-27. Cable Data-Continued

(

(

38 6 4 (branched) 1 6 60 38 5 54 25 1 5 54 25 60 1 6 54


~

I\

cit w

U>

~

(')

Cable

{


28W6 28W8 28W9 28W10 32W10 42Wl 42W2 42W3 42W4 42W5 42W6 42W7 42W8 42W9 42W10 42W13 42W14

(

I

(

11039275 11039276 11039277 11039278 11051227 10576322 10576323 10576324 10576325 10576326 10576327 10576328 11025752 11025815 10576331 11028496 11028978

Reference No.

25 25 25 25 2.6 12 12 12 12 12 12 12 12 12 12 3 4.5

Length (ft.)


{

(

60 54 60 5 1 60 60 60 60 60 6 60 38 60 6 60 (branched) 1 4


(

~

I

~

~

0

~

'°u,

{,

42W50 42W54 42W54 43W6 43W9 43W10 58Wl 60W3 60W9 60W9 60W10 60W10 60Wll 60Wll 60W12 60W12 60W16

Cable

{

{

11039279 11039280 11039299 11039281 11039282 11039283 11039284 11039255 11039256 11039300 11039257 11039301 11039258 11039302 11039259 11039303 11039260

Reference No.

50 50 50 50 50 50 50 35 40 40 40 40 40 40 40 40 5

(

Length (ft.)


(

4 60 60 4 60 4 4 6 60 60 60 60 60 60 60 60 4

{


I

/

'

er. c.n

U>

~

(')

Cable

60W17 60W18 60W20 60W21 60W25 60W32 60W32 60W34 60W34 60W37 60W38 60W40 60W40 60W43 60W44 60W44 60W56

(

(

(_

11039261 11039304 11039262 11039263 11039264 11039265 11039305 11039266 11039306 11039267 11039268 11039269 11039307 11039270 11039271 11039308 11039272

Reference No.

5 500 150 20 16 45 45 40 40 21 12 40 40 100 100 100 25

Length (ft.)


(

{

60 9 4 4 4 60 60 60 60 4 4 60 60 9 25 25 7


(

~

I

',

.i:.

n

°'

c:n

U>

1

{

(

Values for main branch only.

60W101 60W103 60W105 60W108 60W109 60W110 60Wlll 60W112 60Wl 14 60Wl 15 69Wl 69W3 76W3 98Wl 98W2 98W3

Cable

{

11039201 11039203 11039221 11038614 11039209 11039210 11039211 11039212 11039214 11038590 11039289 11039290 11028552 11039204 11039205 11039297

Reference No.

50 35 550 22 150 50 35 35 22 12 50 50 2.2 10 10 2.5

{

Length (ft.)


(

1 2 14 4 4 4 5 5 4 4 4 6 25 60 60 9

{


I

~

\

r

NOit, CAlll QAtdS All llNUTED CAllU IUS !HAN Q.S INCH IN Dl....Slll.

'°'

..,_.

Figure 9·6. Typical multiconductor electrical cables.

C4

9-57 /(9·58 blank)

,,;?"'

1'

____, /

CHAPTER 10 SYSTEM COMPONENTS.TEST STATION (CONTENTS) Item CMTS confidence tests program data ................................................... SCTS interior (auxiliary equipment), left side ........................................... .. SCTS interior (auxiliary equipment), right side ........................................... SCTS interior (major assemblies), left side ............................................ . SCTS interior (major assemblies), right side ......................................... .. SCTS shelter physical data ................ .. SCTS transportation data ................... . Tabulated data ................................... .. UUT test set up data ............................

Reference Table 10-2

Page 10-151

Fig. 10-6

10-9

Fig. 10-5

10-8

Fig. 10·4

10-7

Fig. Fig. Fig. Par. Table

10-3 10·1 10-2 10-1 10-1

10·6 10·4 10·5 10·31 10·10

I

C4

10-1/(10-2 blank)

CHAPTER 10 SYSTEM COMPONENTS TEST STATION 10-1 . Tabulated Data. a. Input Requirements. SCTS power entry panel. ....... 28v de, 65 amp; l 20/208v, 400 Hz, 3·phase, 100 amp/ phase PTS power cab le entry panel. ........... 28v de, 35 amp; 120/ 208v, 400 Hz, 3 ·phase, 50 amp/phase High.pressure air .............. ................. ... .... .. .. ... 3,000 psig

._,

b. Towing Speed Limitations. Imp roved roads and highways ... ........... 50 mph (80 kmph) Unimproved roads .. ... ... .. ....... ... .. ......... 30 mph (48 kmph) Ro ugh ter ra in and poor roads .. .......... ....... 5 mph (8 kmph)

10-3

n

.;..

0

...

I

\

I

1

HOIST POINTS (TYP, BOTH SIDES)

5 T IEDOWN POlNTS (TYP, EACH SIDE) 1,000 LB (453.6 KG) EACH LIMIT LOAD (AIRCRAFT ONLY) 395.25 IN. (10.04 M)-

Figure 10 -1. SCTS shelter physical data.

KINGPIN-8,026 LB (3,641 KGl

LJ:

L_l49.25 lN. I r--- (3=380M) 701N.__, ,. 234.88 IN. ( 1.78 M:) FRONT VIEW 5 97 306 .75 lN. < · Ml NOTE: WEIGHTS: VAN-16 ,495 LB 79 M) (7. TIEDOWN POINTS (7 ,482 KGi 22,000 LB (9 ,979.2 KG) REAR AXLE-6,014 L B (2.728 KG). EACH LIMIT LOAD LANDING GEAR-10 ,481 LB (4,754 KG)

16 IN. (0.41 M)

TIEDOWN POINTS 27,500 LB ( I2,474.2 KG) \I_ EACH LIMIT LOAD [

2 TlEDOWN POINTS (TYP, UNDER BOTH SIDES) 00 LB (2,903.04 KG) EACH LIMIT LOAD

FSNB - 9A I

PINT LE LIMIT LOAD 46, 000 LB (20,865.6 KG)

132 IN. (3.3 5 M)

n

UI

...~

N

{

{

558 IN. (14.17 M)

(

Figure 10-2. SCTS transportation data.

NOTES: 1. WEIGHT:33,496 LB. (15,194 KG). 2. TURNING RADIUS:42.5 FT. (12.95 M) •

( (

(

~

FSNB ... IOBI

l

}

....

w

C')

Cn

0

(

(,

{

(

Figure 10-3. SCTS interior (major assemblies), right side.

TAPE STORAGE CABINET AND WORKTABLE

(

{

)

\

.:..

.... 0

n

(

~

~ ,r

(

(

(

FSNB-40AI

AIR CONDITIONING UNIT 3, 20,000 BTU EACH

(

Figure 10-4. SCTS interior (major assemblies), left side.

(

~

w

n

Co

0

...

{

{l

TEST DOli.Y

{

{

Figure 10-5. SCTS interior (auxiliary equipment), right side.

120V AC CONVENIENCE OUTLET

(

(,

FSNB-39BI

HAND LANTERN

)

~

0 ID

.....

()

INOl SHOWN1

INVERTER FIXIURE

ROfAJtY

FSNU·JBA

PORIABI E HEA IER J

REIURN.AIR REGIS I ER 13/

Figure 10-6. SCTS interior (auxiliary equipment) , left side.

CABl E DUCT COVER fflUSHJ

CONDlllONED·AIR DUCI

(

I

~

(")

0

...~ ...

(

(

I0588880 I0589300 I0596906 I0607305-I I0607305-3 I0608279 I0608280

ioltage monitor module Program generator Rotary inverter Relay Relay Electronic timer Electronic timer

{,i

I05609II I0564660 I0564702 I05647I4 I05647I5 I05647I6 I0564717 I0569489 I0577IOI I0586500

Part No.

ioltage regulator Power distributor :;ontrol computer )C amplifier Jemodulator Isolation amplifier :;apacitor assembly Main distributor "daption kit simulator Guidance computer

Assembly name

-------

-------------

.......

8AIOAI9 -······ 8A4,95A9

28AI BAIO

BAI

.......

8A11AI 8A2 8All 8AI IA2 thru A6 8AI IA7 thru A9 SA I IA IO

Reference designation

{

II035778 I 1035778 I 1035775 11035783 11035783 I1035783 II035783

I 1035775 I 1035775 I I035775 II035775 II035778 I I035775 II035775 I 1035775 II035775 11035778

Tape Container No.

Table 10-1. UUT Test Set Up Data

(

I44 I03 106 I42 I43 I40 I4I IOI,1 I I 110 I05,115,I25, I35 I46 I47 I02 620 623 6I2 624

Program No.

(

95W27 95WI2 95W8 95W27 95W27 95W27 95W27

95W27 95W5 95WIO 95W27 95W27 95W27 95W27 95W7 95W6 95WI3

Cable

/''

I

'\

....0 ....

.... 0

n

Assembly name

1

1103 5776

..... 26

27

Tape No. 1

Tape numbers depicted by l 10 357 XX; e.g., ac stimul i tape num be r is 1103 57 30 .

1 103 5777

Container No.

-----


700

710

Program No.

95W41 thru 95W44

Cable

Table 10-1.SCTS UUT Troubleshooting and Maintenance Data Tests-Continued

Programm ing tape and con tainer (assembly tester executive) Programmin g tape and container (assembly tester selftest)

("

r I

--.\

.... 9 .... ....

~

(")

(

s pecial loads card

Resistive load

Diode assembly

High power loads Accelerometer simulator AC stimuli Relay tree card AC current sensor Non-latching relay card

l ow power loads

Relay assembly Relay Hydraulic actuator

servoamplifier module servoamplifier

Assembly name

{

(

(

11035075 11035220 11035260 11035275 11035305 11035310 11035315 11035320 11035325 11035330

10610100 or 10610150 10610800 10611741 10630142-1/-3 10641100

Part No.

95A3A214

-------

........ .........

.......

.......

lOAlO,Al 1,Al2 and llAlO,All, Al2 95A3A3 95A3A4 95A3A202 95A3A5

-------

.......

8AlOA9,All, A13,Al4,Al6 8A34


304,314,324 303 307 301,321 343 352 354 353 346 341

104 145 610 107

11035775 11035775 11035783 11035775 11035781 11035782 11035782 11035780 11035779 11035779 11035779 11035779 11035779 11035779

150

Program No.

11035778

Tape Container No.

Table 10-1. UUT Test Set Up Data-Continued

(

Cable

95W32 95W31 95W28 95W25 95W27 95W27 95W27 95W27 95W27 95W27

95W9 95Wll 95W27 95Wl9

95W27

(

~

"'

~

0

N

.=..

....0

(,

(

Ladder network card DC stimuli regulator card Master control panel Power relay card Counter measurements card Beta simulator card Special stimuli R-Z measurements card Electro pneumatic test set Pneumatic control panel DC stimuli Card/relay test panel Card/relay test panel EL control box Relay Relay Relay

Assembly name

{

-------------

{

(

340 342 344 311 310 302 306 316,326 401,411 611 614 621

95A3A216 95A3A208 95A3A197 95A2A2 95A2Al 95A3A164,A184 95A3A2 95A3A6 97A1Al ..........

11035355 11035360 11035365 11035375 11035396 11035450 11035491 11035946 11038235 11040047 11040323 11040606

11035780 11035779 11035782 11035782 11035782 11035780 11035782 11035782 11035783 11035783 11035783 11035783

347 350 305 351 345

Program No.

95A3A171.A191 11035779 95A3Al 72,Al92 11035779 95A3Al 11035782 11035779 ----·-95A3A179 11035782

Tape Container No.

11035335 11035340 11035343 11035345 11035350

Part No.



{

95W27, 47 95W27 95W27 95W30 95W29 95W26 95W27 95W27, 47 95W34 95W27 95W27 95W27

95W27 95W27 95W33 95W27 95W27

Cable

~

I

~

w

..:..

.... 0

.c:-

(')

(

(

11051425 11052421

11052702 11052800 11053140 MISl 7300 MISl 7309

Computer power supply Tape reader Remote firing box Teleprinter EL 26 volt power supply

11051290 11051320 11051420 (95A) 32AlA2AlZ33 (95A)32A 1A6 (95A)32A3A4 32A4A10Al 32A3A8 97PS1

-----··

-------------

(95A) 32A2A7Alll 82Al4

541 511 512 502 506 501 405

11035782 11035775 11035780 11035780 11035780 11035780 11035780

507 543 544

11035783 11035782 11035782

505

503

542 540

11051130

(

Program No.

11035782 11035783

11035783

(95A)32A3A2

'11051120

-------

11035780

(95A)32A3A7

Part No.

11051160 11051170

Tape Container No.



(

Azimuth laying control box Filter and test Attenuator limiter and amplifier Comparator and amplifier Oscillator assembly

Azimuth laying control panel Voltage-phone monitor panel Negative bit generator -65 volt power supply

Assembly name

{

Cable

95W18 95W17 95W22 95W16 95W37

95W27, 47 95W14

95W24 95W27, 47 95W27, 47

95W27, 47 95W27

95W21

95W23

(

~

I

'

0 ol:lt

.... 9 .... ol:lt

{

MS25327Dl

Relay

{,,

MIS17317

(

-------

95A3A9,A10, All

97A1A2A5 97 A1A2Al,A3

(

11035783

11035782

622

312

440 442 443

-------

MISl 7314 MISl 7315 MISl 7316 11035779 11035779 11035779

402 441

11035780 11035779

··-----

·····--

MISl 7313

-------

404 403

(

Program No.

11035780 11035780

Tape Container No.

97A2 97A1A2

MISl 7310 MISl 7311

Part No.

EL level sensor Electronic control amplifier level sensing system level signal sensor amplifier EL power supply Amplifier-de mo du Iator leveling amplifierdemodulator 12/14/28v de power supply

Assembly name



(

95W27

95W15

95W39 95W39 95W39

95W38 95W39

95W36 95W35

Cable

/

f

U1

.....
~

(")

Servoamplifier Modulator-demodulator Current driver rrequency and constant monitor Monitor module Mat rix driver Capacitor module - 24-volt power supply Programmable power supply XI Z torquer Y torquer Relay card Volta ge sensor Test driver Load simulator Pulse sequencer and detector

Assem bly name

(

11053110 11053110 11053 11 0 11053110 11053110 11053110 11053110 11053110 11053110 11053110 11053110 11053110 11053110 11053110 11053110 11053110

11051220 11051230 11051235 11051240 11051250 11051255 11051265 11051275 11051295 1 105 1310 11051315 11051330

Contai ner No.

11051155 1105 1 165 11051185 11051190

Reference No.

11053060 11053060 11053060 11053060 11053060 11053060 11053060 11053060 11053060 11053060 11053060 11053060

11053060 11053060 11053060 11053060

Tape No.

A27 A27 A28 A28 A26 A27 A27 A27 A27

cc

M MD

A27 A27 A27 A27

Test co nnector

Table 10-2. CMTS Confidence Tests Program Data

(

78 79 80

77

83 82 84 66 76 69 70 71

61 68 75 67

Test code

24VP CPPS XZTQ YTRQ RELY VSNS CMDC CUT CPSD

cc

MOMO MATO

SRVA MOOD CUDR FCMO

IR I display

I

'

.s::.

(')

en

..... 9 .....

(

(

11053110 11053110 11053110 11053110 11053110 11053110 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865

11051796 11051887 11051920 11053045 11053105 11053159 11052401 11052402 11052403 11052404 11052405 11052406 11052407 11052408 11052409 11052410 11052411 11052412

Load module Command module HEFU timer Reed relay card Telephone amplifier Dual modulator-demodulator Flip-flop module Multiplex module Adder carry chain module Adder module Parity module Register module Driver and gate module Flip-flop module Controls module Comparator module Decoder module Gate module

(/

Container No.

Reference No.

Assembly name

(

11053060 11053060 11053060 11053060 11053060 11053060 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815

Tape No.

(

MD CM A27 A26 A27 A27 A29 A29 A29 A29 A29 A29 A29 A29 A29 A29 A29 A29

Test connector

{

LM CM-L HEFU RDRL TELA DMOD HY101 HY102 HY103 HY104 HY105 HY106 HY107 HY108 HY109 HYllO HYl 11 HYl 12

87 81 74 60 73 86 1 2 4 5 6 7 8 9 10 11 12

3

IRI display

Test code

Table 10·2. CMTS Confidence Tests Program Data-Continued

/

~

=-

-

m

!!:

°'N

9 ....

....

........

-

....~

.... 9 ....

w

(')

(

(

{

11035775 11035778 11035783 11035783 11035775 11035783 11035779 11035779 11035779 11035779 11035779 11035779 11035783 11035783 11035783 11035779

10564717 10589300 10607305-1 10608279 10611741 10630142 11035305 11035310 11035315 11035320 11035325 11035345 11040047 11040323 11040606 MIS 17313/1

Capacitor assembly Program generator Relay Electronic timer Relay assembly Relay Relay tree ca rd AC current sensor Non-latching relay card Diode assembly Resistive load Power relay card Relay Relay Relay Level signal sensor amplifier


97AlA2A2. A4

Container No.

Reference No.

25 28 33 33 25 33 29 29 29 29 29 29 33 33 33 29

Tape No. 1

Cable

95W27 95W12 95W27 95W27 95Wll 95W27 95W27 95W27 95W27 95W27 95W27 95W27 95W27 95W27 95W27 95W39 141 147 620 612 145 610 343 352 354 353 346 351 611 614 621 441

(

Program No.

Table 10-7. UUT's Without Programed Halts (UUT Confidence Test)

(

Assembly name

(

)

I

'

....
C)

~

Container No. 11051865 1 1051865 11051865 11 051865 1105 1865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865

Reference No.

11052413 11052414 11052415 110524 16 11052417 11052418 11052419 11052420 1105242 2 11052423 11052 424 11052425 11052426 110524 29 110524 32 1105 2433 110524 34 11052435 11052436

Assembly name

Multiplex module Controls module Controls module Buffer module Mult iplex module Multiplex module Gate module Gate module Output level changer Input level changer Diode gate ca rd Lamp driver modu le Driver module Positive OR detecto r Sense amplifier / inhibit driver Address decoder / core driver Address buffer modulator Curren t stabilizer modulator Strip printer driver

1105181 5 1105 1815 11 05 18 15 110518 15 1105 1815 1105 1815 11051815 110 51815 11 0518 15 1105 18 15 1 10518 15 11051815 1 1051815 110 518 15 11051815 11051815 11051815 11 05 18 15 11051815

Tape No. A29 A29 A29 A29 A29 A29 A29 A29 A29 A29 A29 A30 A30 A29 A30 A30 A30 A30 A29

Test connector 13 14 15 16 17 18 19 20 22 23 24 25 26 29 32 33 34 35 36

Test code

Table 10-2. CMTS Confidence Tests Program Data -Continued

(

HY113 HYl 14 HY11 5 HY116 HYl 17 HY118 HY 11 9 HY120 HY122 HY1 23 HY124 HY125 HY126 HY129 HY 132 HY133 HY134 HY135 HY 136

IR I display

I

~

0

00

9

--

{

(

11052437 11052438 11052439 11052812 11052817

Test drive card Timing and control A Timing and control B Read amplifier module Control circuit module

()

Reference No.

Assembly name 11051865 11051865 11051865 11051865 11051865

Container No.

(

11051815 11051815 11051815 11051815 11051815

Tape No.

(

A29 A30 A30 A30 A30

Test connector 37 38 39 27 28

Test code

Table 10-2. CMTS Confidence Tests Program Data-Continued

{

HY137 HY138 HY139 HY127 HY128

IRI display

~

I

.'\

'°

...c;:» ...

fl

(

(

{

Reference No.

11051796 11051887 11051920 11053045 11053159 11052401 11052402 11052403 11052404 11052405 11052406 11052407 11052408 11052409 11052410 11052411 11052412

Load module Command module HEFU timer Reed relay card Dual modulator-demodulator Flip-flop module Multiplex module Adder carry chain module Adder module Parity module Register module Driver and gate module Flip-{lop module Controls module Comparator module Decoder module Gate module 11053110 11053110 11053110 11053110 11053110 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865

Container No.

Test connector

MD CM A27 A26 A27 A29 A29 A29 A29 A29 A29 A29 A29 A29 A29 A29 A29

Tape No.

11053060 11053060 11053060 11053060 11053060 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815

IRI display

LM CM-L HEFU RDRL DMOD HYlOl HY102 HY103 HY104 HY105 HY106 HY107 HY108 HY109 HYllO HYlll HY112 87 81 74 60 86 1 2 3 4 5 6 7 8 9 10 11 12

( Test code


{

Assembly name

(

)

•

'

n ...,

N 0

...~

(\

(

11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865 11051865

11052413 11052414 11052415 11052416 11052417 11052418 11052419 11052420 11052422 11052423 11052424 11052425 11052426 11052429 11052432 11052433 11052434 11052435 11052436

Multiplex module Controls module Controls module Buffer module Multiplex module Multiplex module Gate module Gate module Output level changer In put level changer Diode gate ca rd Lamp driver module Driver module Positive OR detector Sense amplifier/inhibit driver Address decoder/core driver Address buffer modulator Current stabilizer modulator Strip printer driver

(

Container No.

Reference No.

Assembly name

{

(

HYl 13 HYl 14 HY115 HY116 HY117 HY118 HYl 19 HY120 HY122 HY123 HY124 HY125 HY126 HY129 HY132 HY133 HY134 HY135 HY136 13 14 15 16 17 18 19 20 22 23 24 25 26 29 32 33 34 35 36 A29 A29 A29 A29 A29 A29 A29 A29 A29 A29 A29 A30 A30 A29 A30 A30 A30 A30 A29 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815 11051815

{

IRI display

Test code

Test connector

Tape No.


~

I

\

.....

N

0

.....

(')

Refere nce No.

11052437 11052438 11052439 11052812 11052817

Assembly name

Test drive card Timing and control A Timing and control B Read amplifier module Control circuit module 11051865 11 051865 11051865 11 051865 11051865

Container No. 110518 15 1105 1815 1105 1815 1105 1815 11051815

Tape No. A29 A30 A30 A30 A30

Test connector 37 38 39 27 28

Test code

Table 10-8. CMTS Conf idence Tests Program Data- Continued

HY137 HY 138 HY139 HY127 HY128

IRI dis pl ay

I

r -

w

CHAPTER 11 SHOP SETS (CONTENTS) Item

Reference

Page

Electrical repai r shop ...................... . General ......................................... . Mechanical repair shop .................. .. Preservation and packaging shop .... .. Supply office ................................. .. Tabu lated data .............................. .. Test equipment stored but not used in electrical repair shop ............ .. .. . Type I repa ir parts shop .......... ... .... .. Type II repa ir parts shop .......... ...... .. Typica l shop set shelter physical data ........... ................................ .

Par.11 ·4 Par. 11 ·1 Par.11 ·3 Par. 11 ·5 Par. 11· 2 Par. 11·8

11-3 11 -3 11 -3 11 ·4 11 ·3 11·4

Table 11 -1 Par.11 ·6 Par. 11 ·7

11·5 11-4 1 1-4

Fig. 11·1

11·6

-

II

11-1

~-

.....--..

'w'· ·..

--

C..V· .

r CHAPTER 11 SHOP SETS 11-1 . General.

..._,

The shop sets consists of 10 individual shelters: a supply office, mechanical repair shop, electrical repair shop, preservation and packaging shop, three type I repair parts shops, and three type II repair parts shops.

11-2. Supply Office. l,._J

The supply office provides the facilities and contains the materials for direction and control of OS and GS mainte· nance operations. The supply office contains two bookracks, a bulletin board, a card file, a fi!e safe, office desk and chair, storage cabinet, visual card index file, and type· writer.

11-3. Mechanical Repair Shop. The mechanical repair shop is used by maintenance personnel to support the OS and GS maintenance capability within the using organization. Tools in the shop are used to perform maintenance operations such as grinding, drilling, lubricating, straightening or bending, repairing stripped tapped holes, replacing helicoil inserts, painting, riveting, and removing and installing press-fit pieces. The shop contains a mechanical shop tool set, mechanical and structures tool set, hydraulic jack tool set, pressure gage tester, torque analyzer tool set, pneumatic maintenance test set, and hydrostatic tester.

11-4. Electrical Repair Shop. The electrical repair shop is used by maintenance personnel to support the OS and GS maintenance capability within the using organization. Test equipment and tools in the shop are used to troubleshoot and repair electrical assemblies, subassemblies, and chassis. The shop contains an electrical shop tool set, electrical cable insulation repair kit, cable tester and adapters, and digital repair tool set. Table 11 • l lists the test equipment that is stored but not used in the electrical repair shop.

C2

11-3

I

11-5. Preservation and Packaging Shop.

I

The preservation and packaging shop provides the facilities and contains the materials required for processing or deprocessing items of equipment for shipment and storage. The shop contains common tools, a steel strapping dispenser, hand steel strapping tensioner, hand steel strapping sealer, an oven, electric hand sealer, portable air extractor, stencil cutting machine, and stencil applicator.

"-"'

11-6. Type I Repair Parts Shop. The type I repair parts shop provides storage facilities for small items such as spare printed circuit cards, resistors, and capacitors.

11-7. Type II Repair Parts Shop. The type II repair parts shop provides storage facilities for spare assemblies, subassemblies, and chassis used to repair the.missile and ground support equipment.

11-8. Tabulated Data. Power requirements: Voltage .............................. 120/208v, 3-phase, 400-Hz 28v de {electrical and mechanical repair shops) Current drain ............ 30 amp average, 60 amp maximum Air conditioner {except type I and II repair parts shops): Power input ................ 208v, 3-phase, 400-Hz at 40 amp Output ........................................................ 50,000 Btu

11-4

Cl

'-'

r

Table 11·1. Test Equipment Stored but Not Used in Electrical Repair Shop Nomenclature

Reference No.

\

TM reference

'.-' Battery test actuator Cable shield resist· ance test set Cable tester ~

\.I

Case vent safe and arm test set EL Electrical circuit test set Electrical filters test set Exploding bridgewire test set Guided missile electrical circuit test set Igniter circuit tester Low resistance ohmmeter test set

C4

11028283 11039161

9-1410-375-35 9-1400-377-34

AN/GSM-45 11028637

9-1430-380-14 9-1400-377-34 9-1410-375-35

11039251

9-1440-380-14

11036000 11028557

9-1427-380-34/1 9-1440-380-14 9-1400-377 .34 9-1410-375-34/1

10560776

9-1410-375-34/1

10055154 11036032

9.4935.379.34 9-1430-380-14 9-1400-377-34

11-5

I

n

°'

.... ....

(,

(

{

29. 50 IN. M) -,...._i..,.~.....,_;....-~-(0.75

1. 75 IN• .------++-(0. 04 M) TYP

POINTS (TYP 4 PLACES)

urTA~ZI

IN.---..i 12.15 Ml I

(

{

{

FSNB·3AI

~ TYP BEARING SURFACE BEARING SURFACE 140.50 IN. (3.57 M) X 146,50 IN. (3. 72 M) X 1.12 IN. (0,03 M) 1.12 IN. (0.03 M)

L

~84.75

Figure 11-1. Typical shop set shelter physical data.

NOTES: 1. MAX LOADS LIFT 11, 000 LB (4,989.6 KG) ANY DIBECTION. TIEDOWN 10, 000 LB (4, 536.0 KG) ANY DmECTION. 2. APPROXIMATE GROSS WEIGHTS. PRESERVATION & PACKAGING - 5,303 LB (2,405 KG). SUPPLY OFFICE - 5,772 LB (2,639 KG). REPAIR PARTS I - 6,086 LB (2,760 KG). REPAIR PARTS II -5,657 LB (2,563 KG). ELECTRICAL REPAIR -4,502 LB (2,042 KG). MECHANICAL REPAIR - 5,376 LB (2,439 KG).

M)

81.38 IN.

-·-1

~L==:=::::===I=:::::::!===~:!....]

(4, . . M)

:I

188.50 IN. (4.79 M) 14------ !~9! ~ ~·----~

~

\

CHAPTER 12 POWER STATION EQUIVALENT (CONTENTS) Item AC generato r set physical data .... .... .. Facilities d istribution trailer physical data .. ............ ............................. . General ......................................... . Tabulated data ....... .................... .... .

Reference

Page

Fig. 12-2

12-5

Fig. 12·1 Par. 12· l Par. 12-2

12-4 12-3 12-3

II

12-1

CHAPTER 12 POWER STATION EQUIVALENT \.,.I

12-1. General. The power station equivalent (PSE) consists of one facilities distribution trailer and two 45-kw ac generator sets.

12-2. Tabulated Data. a. Facilities Distribution Trailer. Weight ............................................. 5,405 lb (2,452 kg) I Motor rating ............................ 15 hp at 6,000 rpm, 208v, 400 Hz, 3-phase DC generator rati"ng ..................... 300 amp, 30v de, 5,700 to 6,300 rpm Voltage adjustment range ................................ 26 to 34.5v Regulation at constant load .................................... ±0.5% Air compressor discharge pressure ................... 3,000 psig Air storage bottle volume ................................ 2,570 cu in. ( 42, 148 cu cm) Air storage bottle operating pressure ................. 3,000 psig

b. AC Generator Set. Weight (includes 58Wl) .................... 6,630 lb (3,007 kg) Generator set ........................... Diesel-engine-driven 45 kw

C3

12-3

w

n

Ja.

N

...

(

- (88.2.240 IN.M)

('

·---, I I

I,, (0. 85 M)

II 33.I5 IN.

~

LIFT AND TIEDOWN POINT (2 PLACES AT REAR)

19. 0 IN. (0. 48 M)

I

{

(

(

:

(

FSNB-GBI

I

J 67. 0 IN. ·- (1.70 M) ·

56. 5 IN, ;.o- (1. 44 M)

(0,35 M)

. 13.G2 IN.

I

Figure 12-1. Facilities distribution trailer physical data.

NOTES: 1. WEIGHT: 5,405 LB (2,452 KG). 2. MAX TIEOOWN LOAD: 5,000 LB (2,268 KG) IN ANY DIRECTION.

Il

(2. 90 M)

BOTH SIDES)'

- - - 168.5 IN. _ (4.28 M)

-

14-- 114. 3 IN.

TIEDOWN POINT (TYP,

~

'\

UI

.... N

n

LIFT

'A'I

I

(S.l::: 11,

I

1

I~

+

(2.36M)

I 28. l IN. 59. 0 IN.

I

20. 0 IN. (O.Sl M)

Figure 12-2. AC generator set physical data.

99.12 IN, (2.52 M)

. 40. 0 IN. (1 . 02 M)

FSNB-7AI

(0.44 M)

17.25 IN.

NOTES: 1. WEIGHT: 6, 630 LB (3, 007 KG). 2. MAX TIEDOWN LOAD: 5, 000 LB (2, 268 KG) IN ANY DIRE CT ION.

,.LIFT POINT (TYP, BOTH SIDES)

~~· :=J-1

69. 5 IN. (1.77 M) 93. O IN.

- -----r-

RJ~Jt

169.SIN.~

4 31 125. 5 IN. < • M) ~--

~~~:g:~r1=.-=-=Eor-t--.=~=r===(O.,!M);L1;~1:r.·

(

r

- - ,,

CHAPTER 13 VEHICLES (CONTENTS) Item

Reference

Page

Tabulated da ta ............... ............. ... . Tractor XM7 5 7 physical data ........... . Truck M656 physical data .... ... ........ .

Par. 13-1 Fig. 13-2 Fig. 13- 1

13-3 13-9 13-8

I

13-1

~ ..

'

w

...w

w

(')

(

W/cargo bows ..............

Height: Overall .........................

b. Dimensions.

Off highway ..................

Payload, max: On highway ..................

Weight, empty .................

a. General.

13 -1 • Tabulated Data •

(

(

9.67 ft (2.95 m)

M656

20,000 lb (9,072 kg) 10,000 lb (4,536 kg)

M656 16,510 lb (7,489 kg)

8.88 ft (2.71 m)

XM757

16,380 lb (7,430 kg)

XM757

CHAPTER 13 VEHICLES

{

9.79 ft (2.98 m)

M55

20,000 lb (9,072 kg) 10,000 lb (4,536 kg)

M55 24,064 lb (10,915 kg)

( (

9.05 ft (2.76 m)

M543

12,000 lb {5,443 kg) 7,000 lb (3, 175 kg)

M543 34,440 lb ( 15,536 kg)

)

'

nw

.;.

...w

{

Floating

Fording depth ..................

{

('

Cable length .................

Front winch: Capacity .......................

M656 50 mph (80 kmph}

8.88 ft (2.71 m) 24.92 ft (7.60 m) 8.0 ft (2.44 m) 12.0 in. (30.5 cm) 42.5 ft (12.95 m) 12.33 ft (3.76 m)

Speed, max .....................

c. Performance.

Wheelbase ......................

Turning circle (radius) .....

Ground clearance ............

Width .............................

Length ............................

W/O cargo bows ..•........

M656

XM757 50 mph (80 kmph) 40 in. ( 102 cm)

24.83 ft (7.57 m) 8.0 ft (2.44 m) 12.0 in. (30.5 cm) 42.5 ft ( 12.95 m) 12.33 ft (3.76 m)

XM757

(

{

20;000 lb (9,072 kg) 200 ft (61.0 m)

M55 50 mph (80 kmph) 30 in. (76 cm)

32.16 ft (9.80 m) 8.13 ft (2.48 m) 10.5 in. (27 cm) 46.5 ft (14.17 m) 17.92 ft (5.46 m)

M55

{

20,000 lb (9,072 kg) 280 ft (85.3 m)

M543 52 mph (84 kmph) 30 in. (76 cm)

29.08 ft (8.86 m) 8.03 ft (2.45 m) 11.0 in. (28 cm) 46.7 ft (14.22 m) 14.92 ft (4.55 m)

M543

~

I

'

UI

...Cf

fl

(

Cooling system ............... . Crankcase: Gasoline engine ..•......... Diesel engine .............. . Oil filter ..........•............... Differentials (each) ......... . Transmission .................. .

e. Capacities.

Highway ......................... . Cross-country ................. . Mud, snow, sand ............ .

d. Tire Pressure.

Off highway ................. .

Recommended towed load: On highway ................ ..

(

( ( 32,000 lb ( 14,515 kg) 32,000 lb (14,515 kg)

XM757

(

8 qt (7.6 liters) 19 qt ( 18.0 liters)

20 qt ( 18.9 liters)

18 qt (17.0 liters) 15 qt ( 14.2 liters) 2 qt ( 1.9 liters) 12 qt ( 11.4 liters) 9 qt (8.5 liters) (W 10 power takeoff) 11 qt ( 10.4 liters) (W /power takeoff)

M55,M543 44 qt (41.7 liters)

M656, XM757

70 psi 35 psi 15 psi

M55, M543

30,000 lb ( 13,608 kg) 15,000 lb (6,804 kg)

M55

34 qt ( 32.2 liters)

40 psi front - 5 5 psi rear 30 psi front - 30 psi rear 10 psi front - 10 psi rear

M656, XM757

13,000 lb (5,897 kg) 13,000 lb (5,897 kg)

M656

(

-

'

~

(13,608 kg) 15,000 lb (6,804 kg)

30.000 lb

M543

w

(")

°'

...w

(

18 17 16 15 14 13

Radius (ft)

(i

M55, M543 5.25 qt ( 5.0 liters) 78 gal (295.6 liters)

{

0

4,000 4,250 4,550 5,000 5,600 6,300

lb lb lb lb lb lb

( 1,814 ( 1,928 (2,064 (2,268 (2,540 (2,858

kg) kg) kg) kg) kg) kg)

Elevation

WI outriggers

o

{

3,000 3,200 3,500 3,800 4, 100 4.6r

lb lb lb lb lb lb

( 1,361 kg) ( 1,452 kg) ( 1,588 kg) (1,724 kg) (1,860 kg) (2.087 t~)

WI 0 outriggers

Note Insure that M543 engine rpm is 1,600± 50 (no·load) when operating boom.

6.75 qt (6.4 liters) 6.75 qt (6.4 liters) 2.6 qt (2.46 liters) 3. 75 qt ( 3.5 liters) 3. 75 qt (3.5 liters) 3 qt (2.8 liters)

XM757 3 qt (2.8 liters) 160 gal (606.4 liters)

270 ° Rotation.......................... Elevation......................... 0°, 15°, 30°, 40° Boom capacity (2-part hoist line):

f. M543 Boom.

Winch: Front .......................... . Rear ........................... .

Transfer case.................. Fuel tank .. ..... ... ..... ... ......

M656 3 qt (2.8 liters) 80 ga I ( 303.2 liters)

~

'

....

~

....w

n ...,,

{

18 17

18 17 16 15 14 13 12 11 10

lb lb lb lb lb lb lb lb lb kg) kg) kg) kg) kg) kg) kg) kg) kg)

30 ° Elevation

( 1,905 (2,041 (2,223 (2,427 (2,722 (3,004 (3,538 ( 4, 128 ( 4,536

4,950 lb (2,245 kg) 5,450 lb (2,472 kg)

4,200 4,500 4,900 5,350 6,000 6,800 7,800 9, 100 10,000

7' 150 lb ( 3,243 kg) 8,400 lb (3,810 kg) 10,000 lb (4,536 kg)

12 11 10 15 ° Elevation

WI outriggers

(

Radius (ft)

{

(,

{

lb lb lb lb lb lb lb lb lb

(l,406 ( 1,565 ( 1,656 ( 1,814 ( 1,973 (2,200 (2,495 (2,812 (3,221

kg) kg) kg) kg) kg) kg) kg) kg) kg)

3,700 lb ( 1,678 kg) 3,950 lb ( 1,792 kg)

3,100 3,450 3,650 4,000 4,350 4,850 5,500 6,200 7,100

5,100 lb (2.~13 kg) 5,800 lb (2,631 kg) 6,700 lb (3,039 kg)

WI O outriggers

(

~

~

\

n~

N

a.

.... w

{

(

lb lb lb lb lb lb

6,300 6,950 7,SQO 8,900 10,200 11,500

18 17 16 15 14 13 12 11 10

{

lb lb lb lb lb

6,050 6,750 7,500 8,650 10,250

kg) kg) kg) kg) kg)

(2,858 (3,153 (3,538 (3,237 (4,627 (5,216


40 ° Elevation

(2,744 (3,062 (3,402 (3,924 (4,649

WI outriggers

16 15 14 13 12 11 10

Radius (ft)

{

(

4,600 5,000 5,500 6,100 6,750 7' 500

4,300 4,750 5,300 6,000 6,800

lb lb lb lb lb lb

lb lb lb lb lb

(2,087 (2,268 (2,495 (2,767 (3,062 ( 3,402

( 1,950 (2,155 (2,402 (2,722 (3,084


kg) kg) kg) kg) kg)

('

W/O outriggers

/

~

:..,

...w

~

(')

(

(

(

( 32,793 33,480 27, 106 24,747 27,190 22,030 46,546 33,496

{

g. Vehicle Weight With Payload (Approximate). M55W/1st stage in container ....................................................... M55 W/2nd stage and guidance section in containers ..................... M55 W/warhead section in container ............................................. M656 W/PTS·PS .......................................................................... M656 W/BCC .............................................................................. M656 W/RTS .............................................................................. ~ XM757 and EL W/missile .............................................................. XM757 and SCTS ......................................................................... lb ( 14,874 lb (15,186 lb ( 12,295 lb (11,225 lb ( 12,333 lb ( 9,992 lb (21,113 lb (15,193

( kg) kg) kg) kg) kg) kg) kg) kg)

)

I

I

...,

Co

...w

(

r·

E

__....i

('1

(

Figure 13-1. Truck M656 physical data.

(

ll6.0IN. (2.95 M) 106.5 IN. (2.71 M)

(

(

FSNB-12

80.0 IN. (2,03M)

K?~ !'1 IT I

3. TURNING KADIUS: 42.5 FT (12.95 M).

58.0 IN. (l.47 M)

_-+l--..;.·-.....,i

~

D

(~~2~~> __,..,._

148 OIN • 206 • 0 IN. (3.76 M) (S.23 M) 299 IN. NOTES: (7 .59 M) 1. WEIGHT: 16,276 LH (7 ,370 KGl 2. AXLE LOADS: C&D - 2,352 LB (1,068 KG) l!:ACll E&F - 5,786 LR (2,625 KG) EACH

I

I

58.0IN. : (l.47 M ) •

F

AXLE

' I

HOIST POINTS 45,000 LB (20,412.0 KG) CAPACITY TIEDOWN (PINTLE) 20,000 LB (9,072.0 KG) CAPACITY

TIEDOWN POINTS AND LIMIT LOADS TIEDOWN LIMIT LOADS I I TllHU I (TYP, ROTll SIDES)! 6,000 LB (2,721.6 KG) ANY DlllECTION m AND n (TYP, ROTH SIDES) I 15,0UU LB (6 804 KG) ANY DIHECTION

_,)

"'

ID

.... w

(')

(

I~

>.. I

,,........,

AXLE E

II I .1.

(

.'?.:-' ........

I

I

>_J , . . . ._

(

I

I

(

Figure 13-2. Tractor XM757 physical data.

BOTH SIDES)

BOTH SIDES)

ANY DIRECTION

FSNB-llA I

LB (2, 721. 6 KG) ANY DIRECT ION

115. 000 LB (6. 804. 0 KG)

LIMIT LOADS

m AND n (TYP,

J

I 6. 000 I THRU I (TYP,

TIEDOWN

TIEDOWN POINTS AND LIMIT LOADS

58 . 0 IN. ( 1.4? M)

I

(PINT LE) Il'f===ri!t:=~J::l\ 20,000 LB..., (9,072 KG) I CAPACITY +>-L+----+---,f"-:-"""t--'--~

m TIEDOWN

HOIST POINTS 45,000 LB (2, 041 2KGl~I .' CAPACITY

90.0!N . . .,. I . ., I (2.29 M) 58.0 IN. • 148.0 IN. • ( 1.4? M) (3 .16 M) _ _ __ _ _ _206. 0 IN~.------ ( 5.23 M) ~---------~298 . 0IN._ _ _ _ _ _ _ _,... (7 .57 Ml NOTES: I . WEIGHT: 16,966 LB (7 ,655 KG). 2.TURNING RADIUS: 42.5 FT (12.95 M). 3. AXLE LOADS: C & D-2,29? LB (1,042 KG) EACH. E & F- 6 ,186 LB (2,806 KG) EACH.

I

.........

AXLE F

....... I

(

r

CHAPTER 14 PUBLICATIONS (CONTENTS) Item Forms ......................... .. .... .... ......... . Other publications ....................... ... . PERSHING la technical manuals .. .... .

Reference

Page

Par. 14-1 Par. 14-3 Par. 14-2

14-3 14-6 14· 3

I

14-1

r

CHAPTER 14 PUBLICATIONS

~

14-1. Forms. DA Form 2028

Recommended Changes to DA Technical Manuals Parts Lists or Supply Manual 7, 8, or 9

DA Form 2404

Equipment Inspection and Main· tenance Worksheet

DA Form 2415

Ammunition Condition Report

14-2. PERSHING la Technical Manuals. '.-I

a. Azimuth Laying Set. TM 9-1430-378-20P TM 9· 1430-378-34P TM 9-1430-381-14

I

b. Azimuth Laying Training Set. TM 9-6920-378-20P TM 9-6920-378-34P TM 9-6920-381-14

I

c. Battery Control Central. TM 9-1427-381-14 TM 9-1430-383-20P TM 9-1430-383-34P

I

d. Erector-Launcher. TM 9-1440-380-14 1..,.1 TM 9-1440-380-20P TM 9-1440-380-34P

I

e. EL Cable Mast. TM 9-1440-380-14 TM 9-1440-381-20P '..,/ TM 9-1440-381-34P

I

f. EL Electrical Circuit Test Set. TM TM L-1 TM ....... TM

C3

9-1430-380-14 9-1440-380-14 9-4935-385-20P 9-4935-385-34P

I 14-3

g. Handling Equipment and Mounting Sets.

I

TM TM TM TM TM

I

h. Missile. TM 9-1410-375-12 TM 9-1410-375-20P TM 9-1410-375-34/1 TM 9-1410-375-34/2 TM 9-1410-375-35 TM 9-1410-375-34P

I

TM 9-6920-375-20P TM 9-6920-375-35P TM 9·6920-382-14

I

9-1450-379-20P 9-1450-379-34P 9-1450-380-14 9-1450-380·20P 9-l 450-380-34P

i. Missile Training Set.

I I

j. Power Distribution System. 9-1430-380-14 9-1430-380-20P 9-1430-380·34P 9-1430-381-20P 9-1430-381-34P

TM TM TM TM TM

k. Power Station. LO 5-1450-202-12 TM 5-1450-202-12 TM 5-1450·202-20P TM 5-1450-202-34 TM 5-1450-202-35P

I. Power Station Equivalent. LO 5-1450-203-12 TM 5-1450-203-12 TM 5-1450-203-20P TM 5-1450-203-35 TM 5-1450-203-35P m. Radio Terminal Set. TM 11-5820-469·10 TM 11-5820-469-20 TM l l ·5820-469-20P TM 11-5820-469-35 TM 1 l-5820·469-35P TM 11-5820-610-15

14-4

C3

I

n. Shipping and Storage Containers. T M 9·8140-375-20P TM 9-8140-37 5-24 TM 9-8140-375-34P o. Shop Sets.

TM TM TM TM TM TM TM

9-1400-377-34 9-1450-376-34P 9-1450-377-34P 9.4935.373.34p 9.49 35.379.34p 9-4935-380-34P 9-4935 -38 1-34P

p. System.

LO 9- 1400-37 5-20

Lubrication instructions

TB 750-236

Calibration Requirements for the Ma intena nee of Army Materiel

TM 9-1400-379-15

Storage, Surveillance, Preparation for Shipment, and Demoli· tion to Prevent Enemy Use

TM 9-1425-380- L

List of Applicable Publications

TM 9-1425-380-10

Description of the PERSHING la Field Artillery Missile System

TM 9-1425-381-10

Firin g Position Procedures

TM 9-1425-381-10/ 2

Operators Manual for Supervisor

TM 9-1425-381- 10/ 3

Operators Manual for EL OP

TM 9-1425-381-10/4

Operators Manual for Crewman 1

TM 9-1425-381-10 / 5

Operators Manua l for Crewman 2

TM 9-1425-381 -10/ 6

Operato rs Man ua I for Crewmen 3, 4, 5, and 6

TM 9-1425-38 1-10/7

Opera tors Manual for PTS and PS OPS

TM 9· 1425-381·10/ 8

Opera tors Manual for HLT, VL T, and OST OPS

TM 9-1425-381·10/9

Opera tors Manual for CAS and MSL Handlers

q. Test Stations .

TM 9-1425-380-24

C4

Functional Diag ram s and Tactica l Co untdown Program Data

14-5

r

TM 9-1425-381-34

Functional Diagrams for PTS Computer and Electronic Circuit Plug-In Unit Test Set

TM 9-1427-380-12/1

PTS

TM 9-1427-380-12/2

PTS

TM 9-1427-380-20P

PTS and SCTS

TM 9-1427-380-34/1

I I

TM TM TM TM

9-1427 -380-34/2

PTS Wiring Data for PTS

9-1427-380-34P

PTS

9-1430-385-20P

Computer Assembly

9-1430-385-34P

Computer Assembly

TM 9-4935-382-34P

SCTS

TM 9-4935-385-14/1

SCTS

TM 9-4935-385-14/2

SCTS

TM 9-4935-385-14/3

I TM 9-4935-385-14/4

·~

Equipment Tested With SCTS Wiring Data for SCTS

r. Tool Sets. SC-4935-95-CL-A76

Mechanical Shop

SC-4935-95-CL-A77

Electrical Shop

SC-4935-95-CL-A78

Digital Repair

SC-4935-95-CL-A79

Contact Team

SC-4935-95-CL-ABO

Mechanical and Structures

SC-5180-95-CL-A44

Missile Mating

SC-5 l 80-95-CL-A45

Firing Position

s. Vehicles.

LO 9-2320-211-12 TM TM TM TM

9-2320-230-10 9-2320-230-20 9-2320-230-20P 9-2320-230-34 TM 9-2320-230-34P TM 9-2815-210-35

I

t. Warhead Section. TM 9-1100-375-12 TM 9-1100-375-34

14-6

C3

r ~

TM 9-1185-212

EOD Procedures

TM 9-1190-224-15

WS Stand

TM 9-l 190-224-25P

WS Stand

TM 9-1190-225-15

T-4109A

TM 9-l 190-225-25P TM 9-1190-227-35

T-4109A

TM 9-1190-227-35P

T-4127A

TM 9-1190-233-35

WS Trailer

T-4127A

14-3. Other Publications. AR 380-5

Safeguarding Defense Information

AR 385-10

Army Safety Program

"W AR 700-1300-8

Malfunctions Involving Ammunitions and Explosives

FM 21-11

First Aid for Soldiers

LO 9-2330-246-12

lubrication Order: Semitrailer, Van: Electronic, 6-Ton

SB 38-100

Preservation, Packaging, and Packing Materials, Supplies, and Equipment Used by the Army

TB 9-352

Load-Testing Vehicles Used To Handle Missiles and Rockets

TB 9-6685-210-50

Calibration Procedure for: Dial Indicating Pressure Gages ( 0 to 10,000 PSI)

TB 55-46

Standard Characteristics for Transportability of Military Vehicles and Equipment

TB 742-93-1

Inspection and Test of Air and Other Gas Compressors

'..,/ TB 750-111

TB CML 49

'-..I TB ORD 38 5

C3

Calibration Procedures for: Tester, Torque Wrench, Torque Kit Wrench, Wrench Set Torque Reactivation of Desiccants in Bags Standards for Oversea Shipment and Domestic Issue of Ordnance Materiel Other Than Ammunition and Army Aircraft

14-7

r I

TB SIG 222

Solder and Soldering

TM 5-2805-204-14

Engine, Gasoline

TM 5-4120-222-15 TM 5-4120-259-15

Air Conditioner Air Conditioner

TM 5-4120-274-15

Air Conditioner, PTS

TM 5-4520-200-12

Heater, Duct Type, Portable

TM 5-4520-206-15

Heater, Duct Type, Portable

TM 5-4520-209-15

Heater, Space

TM 5-4520-209-25P

Heater, Space

TM 5-4520-211-14

Heater, Space

TM 5-6115-274-12

Generator Set, Diesel Engine: 45 KW

TM 5-6115-299-10

Generator Set, Gasoline Engine: "'-"' 10 KW

TM 5-6115-300-10

Generator Set, Gasoline Engine: 5 KW

TM 5-6115-300-15

Generator Set, Gasoline Engine: 5 KW

TM 5-6115-332-12

Generator Set, Gasoline Engina: 5 KW

TM 5-6115-365-15

Generator Sets, Gasoline and Diesel Engine Driven

I

TM 5-6675-296-12

Theodolite W/Accessories and Tripod

I

TM 5-6675-296-35

Theodolite W/Accessories and"-" Tripod

TM 5-9057

Trailer Chassis, Generator

TM 9-208-1

Cleaning of Ordnance Materiel

TM 9-213

Painting Instructions for Field

TM 9-247

Materials Used for Cleaning, Preserving, Abrading, and Cementing Ordnance Materiel; and Related Materials Including Chemicals ._,,

TM 9-1300-206

Care, Handling, Preservation, and Destruction of Ammunition

14-8

Use~

C3

r TM 9-1375-200

\._/

Demolition Materials

TM 9-2320-209-10

2-1/2-Ton, 6 x 6, Chassis, Truck

TM 9-2320-209-20

2-1/2-Ton, 6 x 6, Chassis, Truck

TM 9-2320-209-35

Cab, Chassis and Body Components for Chassis, Truck: 21/2-Ton,6x6

TM 9-2320-211-10

Truck, Chassis: 5-Ton, 6 x 6

TM 9-2330-205-14

Chassis Trailer: 1/2-Ton

TM 9-2330-246-14

Semitrailer, Van: Electronic, 6Ton

TM 9-4935-282-34

Voltmeter, Electronic

TM 9-4935-378-34

AC/DC Differential Voltmeter

~

'-"TM 9.4935.379.34

Generator, 2-

Igniter Circuit Tester

TM 9-4935-380-34

Electronic Counter

TM 9-4935-381-34

Oscilloscope

TM 9-6625-331-15

Test Set, Electrical Cable: AN/ GSM-45

C3

14-8.1/ ( 14·8.2 blank)

I

TM 9-6625 -236 1-14

Voltmeter, Electronic

TM 9-6625-2362-12

Oscilloscope, Vol II

TM 9 -6625-2362-34

Oscilloscope, Vol I

TM 9-8210

2-1/ 2-Ton, 2-Wheel Chassis Trailer

TM 10-269

General Repair for Ca nvas and Webbin g

TM 11 -530

Installa tion Practices for Aircraft Electr ic and Electronic Wiring

TM 11 -5805-20 1-12

Telep hone Set TA-312 / PT

Generator

TM 11 -5805-20 1-35

Telephone Set TA-312 / PT

TM 11 -5805-262-12

Switchboard, Telephone

TM l l -5805-262-20P

Switchboards, Te lephone

TM 11 -5805-262-35

Switch boards, Telephone

TM l 1-5805-262 -35P

Swi tchboard s, Telephone

TM 11 -5815 -205 -15

Teletypewriter Central Office AN / MGC-17

TM 11 -5 820-284-15

Radio Receiving Set AN / GRR-5

TM 11 -58 20-348-15

Antenna Equipment RC-2 92

TM 11 -5820-40 1-10

Radio Sets

TM 11 -5820-4 01-20

Radio Sets

TM 11 -5820-401-35

Radio Sets

TM 11 -5820-477-12

Radio Set Control Groups

TM l 1-5820- 477 -20P

Radio Set, Control Group

TM 11 -5820 -477-35

Radio Set Control Groups

TM l l - 5965 -222-15P

Loud speaker , Dynamic

TM 11 - 5965-231-15P

Headset, Electrical

TM 11-5965-257-15

Handset

TM 11 -5965-2 62 -13

Headset-M icrophone

TM 11 -6625-2 03-12

Multimeter

TM l l -6625-203-20P

Multimeter

TM 11-6625-203-35

Multimeter

TM l l -6625-2 03 -45P

Multimeter

TM 11-6625-239-12

Electronic Mu ltim ete r s

Cl

14-9

TM l l-6625-239-2 0P

Electronic Multimeters

TM 11-6625-239-35

Electro nic Multimeters

TM l l -6625-239-35P

Electronic M u ltimeters

T M 38-230

Pr eservation, Packaging, and Packing of MilitarySuppliesand Equipment

TM 38-750

Army Equipment Reco rd Procedures

14-10

Cl

CHAPTER 15 CONVERSION TABLES

TO CONVERT

INTO

MULTIPLY BY

A acres ac res acres acres ac re.feet acre.feet amperes /sq cm amperes/sq cm amperes/ sq in. amperes/sq in. amperes / sq meter amperes / sq meter ampere-hours ampere-ho urs ampere-turns ampere-turns/ cm ampere-turns/ cm ampere -turn s/cm ampere-turns/ in. ampere-turns / in. ampere-turns/ in . ampere-turns/ meter ampere-tu rn s/ meter ampere-turns / meter atmospheres atmospheres

sq feet sq meters sq mil es sq ya rds cu feet gallons amp/sq in . amp/ sq meter amp/sq cm amp/sq meter amp/ sq cm amp/ sq in . coulombs fa radays gilberts am p-turns/in. amp-turns / meter gilberts/cm amp-tu rn s/ cm amp-turns/ meter gilberts/ cm amp-turn s/cm

43,560.0 4,047.0 l. 562x10 -3 4,840.0 43,560.0 3.259 x 10 5 6.452 1 o• 0.1550 1 ,5 50.0 10" ' 6.452x 10-• 3,600.0 0 .0373 1 1. 257 2.540 100.0 1.25 7 0.3937 39.37 0.4950 0.01

am p-turn s/in.

0.0254

gil berts/cm

0. 01 257

cm of mercury ft of water (at

76.0 33.90 -

atmospher es

in. of mercury (at

4°C) 29.92

0°c) atmospheres atmospher es atmospheres atmospheres

kg / sq cm kg/sq meter pounds/sq in. tons /sq ft

1.0333 10,332 .0 14 .70 1.058

I 15-1

r TO CONVERT

Btu Btu Btu Btu Btu Btu Btu Btu Btu/hr Btu/hr Btu/hr Btu/hr Btu/min Btu/min Btu/min Btu/min Btu/sq ft/min

INTO B ergs foot-lb gram-calories horsepower-hr joules kilogram-calories kilogram-meters kilowatt-hrs foot-pounds/sec gram-cal/sec horsepower-hr watts foot-lb/sec horsepower kilowatts watts watts/sq in.

MULTIPLY BY

1.0550 x 10 10 778.3 252.0 3.93lx10-4 1,054.8 0.2520 107.5 2.928X 10 - 4 0.2162 0.0700 3.929x 10-4 0.2931 12.96 0.02356 0.01757 17.57 0.1221

c calories, gram (mean) centigrade centigrams centiliter centiliter centiliter centiliters centimeters centimeters centimeters centimeters centimeters centimeters centimeters centimeters centimeter -dyn es centimeter-dynes centimeter-dynes centimeter-grams centimeter-grams centimeter-grams centimeters of mercury centimeters of mercury

15-2

Btu (mean)

3.9685x 10-3

Fahrenheit grams ounce fluid (U.S.) cubic inch drams liters feet inches kilometers meters miles millimeters mils yards cm-grams meter-kg pound-feet cm-dynes meter-kg pound-feet atmospheres

(C 0 x9/5)+32 0.01 0.3382 0.6103 2.705 0.01 3.281x10-2 0.3937 10-s 0.01 6.214X 10-6 10.0 393.7 1.094x 10- 2 i.02ox10- 3 1.020xlo-a 7.376x10-a 980.7 10- 5 7.233X 10 • 5 0.01316

feet of water

0.4461

WI

'-'. _, ~

~ TO CONVERT centimeters of mercury centimeters of '.II' mercury centimeters of mercury centimeters/ sec centimeters/ sec centimeters/ sec ~ centimeters/sec centimeters/ sec centimeters/ sec centimeters/ sec centimeters/sec/ sec 1...,1 centimeters/ sec/ sec centimeters/sec/ sec centimeters/ sec/ sec circular mils circular mils circumference circular mils coulombs coulombs/sq cm coulombs/ sq cm coulombs/sq in. coulombs/sq in. I.._,)

coulombs/sq meter coulombs/ sq meter cubic centimeters 1.,1 cubic centimeters cubic centimeters cubic centimeters cubic centimeters cubic centimeters cubic centimeters ~ cubic centimeters cubic feet cubic feet cubic feet

INTO

MULTIPLY BY

kg/sq meter

136.0

pounds/sq ft

27.85

pounds/sq in.

0.1934

feet/min feet/sec kilometers/hr knots meters/min miles/hr miles/min feet/sec/sec

1.1969 0.03281 0.036 0.1943 0.6 0.02237 3.728x 10-4 0.03281

km/hr/sec

0.036

meters/sec/sec

0.01

miles/hr/sec

0.02237

sq cm sq mils radians sq inches faradays coulombs/sq in. coulombs/sq meter coulombs/sq cm coulombs/sq meter coulombs/sq cm

5.067x10-6 0.7854 6.283 7.854x 10-1 1.036x10-5 64.52 10 4

coulombs/sq in.

6.452x10- 4

cu feet cu inches cu meters cu yards gallons (U.S. liq) liters pints (U.S. liq) quarts (U.S. liq) cu cm cu inches cu meters

3.531X10-5 0.06102 10-6 l.308X 10-5 2.642x10- 4 0.001 2.113x 10-3 l.057X 10-3 28,320.0 1,728.0 0.02832

0.1550 1,550.0 10-4

15·3

r

\ TO CONVERT

I

cubic cubic cubic cubic cubic cubic cubic cubic cubic

feet feet feet feet feet feet/min feet/min feet/min feet/min

cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic cubic

feet/sec feet/ sec inches inches inches inches inches inches inches inches inches meters meters meters meters meters meters meters meters yards yards yards yards yards yards yards yards yards/min yards/min yards/min

days decigrams deciliters decimeters degrees (angle)

15-4

INTO

MULTIPLY BY

cu yards gallons (U.S. liq) liters pints (U.S. liq) quarts (U.S. liq) cu cm/sec gallons/sec liters/sec pounds of water/ min million gal/day gallons/min cu cm cu feet cu meters cu yards gallons liters mil-feet pints (U.S. liq) quarts (U.S. liq) cu cm cu feet cu inches cu yards gallons (U.S. liq) liters pints (U.S. liq) quarts (U.S. liq) cu cm cu feet cu inches cu meters gallons (U.S. liq) liters pints (U.S. liq) quarts (U.S. liq) cubic ft/sec gallons/sec liters/sec D

0.03704 7.48052 28.32 59.84 29.92 472.0 0.1247 0.4720 62.43

seconds grams liters meters mils

86,400.0 0.1 0.1 0.1 17.77777

"'-"

0.646317 448.831 16.39 5.787X l0-4 l.639x 10-5 2.143x 10-5 4.329x10-3 0.01639 1.061x105 0.03463 0.01732 10 6 35.31 61,023.0 1.308 264.2 1,000.0 2,113.0 1,057.0 7.646x 10 5 27.0 46,656.0 0.7646 202.0 764.6 1,615.9 807.9 0.45 3.367 12.74

~

"-"'

~

C3

TO CONVERT degrees (angle) degrees (angle) degrees (angle) degrees/sec degrees/ sec degrees/ sec dekagrams dekaliters dekameters dyne/ cm dyne/ sq cm dyne/ sq cm

....,,

dyne/ sq cm

INTO quadrants radians seconds radians/ sec revolutions / min revolutions / sec grams liters meters erg/ sq millimeter atmospheres inch of mercury at 0°C inch of water at

4°C dynes dynes dynes dynes dynes dyn es

grams joules/ cm joules/ meter (newtons) kilograms pounda ls pounds

em, pica em, pica erg/ sec ergs ergs ergs ergs ergs ergs ergs ergs ergs ergs ergs ergs/ sec ergs/sec ergs/sec ergs/s ec ergs / sec ergs/sec

inch cm dyne - cm / sec Btu dyne -cm foot-pounds gram -calories gram-cm horsepower-hr joules kg-calories kg-meters kilowatt-hrs watt-hours Btu / m in ft-lb/ min ft- lb/sec horsepower kg-calories/m in kilowatts

MULTIPLY BY

0.01111 0.01745 3,600.0 0 .01745 0 . 1667 2 .778x io-1 10.0 10.0 10.0 0.01 9 .869x10 - 1 2 .953x 10-5 4 .015 x 10-• l.020 x 10-1 10- 1

10-5 l.020x 10 - 5 7.233X 10-5 2.248x 10-5

E

...,

0 . 167 0.4233 1.000 9.480x 10-11 1.0 7.367x io-8 0.2389 x 10- 1 i.02o x 10- 1 3 .7250 x 10-1•

io-1

2.389X 10-11 i.02o x io-8 0 .2778x 10-11 0 . 2 7 7 8 x 1 o-to 5 ,688x 10- 9 4 . 427 x l0- 6 7.3756x 10 - 8 1.341x10-10 l.433x 10- 9 io-10

15-5

( TO CONVERT

INTO

MULTIPLY BY

F farads faraday/sec faradays faradays fathoms fathoms feet feet feet feet feet feet feet feet of water feet of water feet of water feet of water feet of water feet of water feet/min feet/min feet/min feet/min feet/min feet/sec feet/sec feet/sec feet/sec feet/sec feet/sec feet/ sec/ sec feet/ sec/ sec feet/ sec/ sec feet/ sec/ sec feet/ 100 feet foot-pounds foot-pounds foot· pounds foot-pounds foot-pounds foot-pounds foot.pounds foot-pounds foot-pounds/min foot.pounds/min

15-6

microfarads ampere (absolute) ampere·hours coulombs meters feet centimeters kilometers meters miles (nautical) miles (statute) millimeters mils atmospheres in. of mercury kg/sq cm kg/sq meter pounds/sq ft pounds/sq in. cm/sec feet/sec km/hr meters/min miles/hr cm/sec km/hr knots meters/min miles/hr miles/min cm/sec/sec km/hr/sec meters/ sec/ sec miles/hr/sec percent grade Btu ergs gram-calories hp-hr joules kg-calories kg-meters kilowatt-hr Btu/min foot-pounds/sec

10 6 9.6500x 104 26.80 9.649X 10 4 1.828804 6.0 30.48 3.048x 10-4 0.3048 1.645x10- 4 1.894x 10-4 304.8 1.2x10 4 0.02950 0.8826 0.03048 304.8 62.43 0.4335 0.5080 0.01667 0.01829 0.3048 0.01136 30.48 1.097 0.5921 18.29 0.6818 0.01136 30.48 1.097 0.3048 0.6818 1.0 1.286x10-3 1.356Xl0 7 0.3238 5.050x 10- 1 1.356 3.24x 10-4 0.1383 3.766x10- 7 1.286 x 10- 3 0.01667

~

~

\w.I

v

...,,

'-""

._

TO CONVERT

INTO

MULTIPLY BY

foot-pounds/m in foot-pounds/m in foot-pounds/min foot-pou nds/sec foot- pounds/sec foot-pounds/sec foot-pounds/sec foot-pou nd s/sec furlongs furlongs

horsepower kg-ca lories/m in kilowatts Btu / hr Btu/ min horsepower kg-calories/min kilowa tts miles (U.S.) feet

3 .030x l0 - 5 3.24x l o - • 2.260x 10-5 4.6263 0.077 1 7 l.8 18x 10- 3 0.0 1945 1.356 x 1 0 - 3 0.125 660.0

G CU·Cm cu feet cu inches cu meters cu yards liters ga llons (U.S. liq)

3,785.0 0.1337 231.0 3.785x10- 3 4.951x10- 3 3.785 1.20095

gallons ga llons gallons gallons ga llons gallons gallons ( liq British Imp.) gallon s ( U.S. ) gallons of water gallons/ min ga llons / min gallons/min gausses gausses gausses gausses gilberts gilberts/cm gil berts/ cm gil berts/ cm gra de grams grams grams grams grams grams grams grams grams grams/ cm gra ms/ cu cm

ga llons (Imp.) pounds of water cu ft/sec liters /sec cu ft/hr lines/sq in. webers/sq cm we be rs/ sq in . webers/ sq meter ampe10e-turn s amp-turns/ cm amp-turns/ in. amp.turns/meter rad ian dynes joules/ cm joules / meter (newtons) kilograms milligrams ounces (avd p) ounces (t roy) poundals pounds pounds/ inch pounds/ cu ft

0 .83267 8.3453 2.228x l0- 3 0.06308 8.0208 6.452 10 ~ 6.452x10 - s lo-• 0.7958 0.7958 2.021 79.58 0 .01571 980.7 9.807x 10- 5 9 .807 x 10- 3 0.001 1,000.0 0 .03527 0.032 15 0.0 7093 2.205x10-3 5.600xl0-3 . 62 .43

15·7

(

\ TO CONVERT

INTO

MULTIPLY BY

grams/cu cm grams/cu cm grams/liter grams/liter grams/liter grams/sq cm gram -calories gram-calories gram-calories gram -calories gram-calories gram-calories gram-calories/sec

pounds/cu in. pounds/mil-foot pounds/ 1,000 gal pounds/cu ft parts/million pounds/sq ft Btu ergs foot-pounds horsepower-hr kilowatt-hr watt-hr Btu/hr Btu ergs joules kg-cal kg-meters

0.03613 3.405x 10-1 8.345 0.062427 1,000.0 2.0481 3.9683X 10-3 4.1868x 10 7 3.0880 1.5596 x 1 o- 6 1.1630x 10- 5 1.1630x 10- 3 14.286 9.297X10- 8 980.7 9.807x 10- 5 2.343x 10-s 10-5

gram~centimeters

gram-centimeters gram-centimeters gram-centimeters gram-centimeters

"-1

~

..,

H hand hectograms hectoliters hectometers hectowatts henries horsepower horsepower horsepower horsepower (metric) (542.5 ft lb/sec) horsepower (550 ft lb/sec) horsepower horsepower horsepower horsepower (boiler) horsepower (boiler) horsepower-hr horsepower-hr horsepower-hr horsepower-hr

15-8

cm grams liters meters watts millihenries Btu/min foot-lb/min foot-lb/sec horsepower (550 ft lb/sec)

10.16 100.0 100.0 100.0 100.0 1,000.0 42.44 33,000.0 550.0 0.9863

horsepower (metric) (542.5 ft lb/sec) kg-calories/min kilowatts watts Btu/hr

1.014 10.68 0.7457 745.7 33.479

kilowatts

9.803

Btu ergs foot-lb gram-calories

2,547.0 2.6845 x 10 13 1.98x106 641,190.0

lw-1

TO CONVERT

~

.....,

INTO

MULTIPLY BY

horsepower-hr horsepower-hr horsepower-hr horsepower-hr hours hours hundredweights (long) hundredweights (long) hundredweights (short) hundredweights ( short) hundredweights (short) hundredweights ( short)

joules kg-ca lories kg-meters kilowatt-hr days weeks pounds

2.684x 10 6 641.1 2.737xl0 5 0.7457 4.167 x 10- 2 5.952x 10-3 112.0

tons (long)

0.05

ounces (avoirdupois) pounds

1600.0 100.0

tons (metric)

0.0453592

tons (long)

0.0446429

inches inches inches in ches inches inches inches of mercury inches of mercury inches of mercury inches of mercury inches of mercury inches of mercury inches of water (at 4 °C ) inches of water (at 4°C) inches of water (at 4°C) inches of water (at 4°C) inches of water (at 4°C) inches of water (at 4°C) internationa I ampere

centimeters meters miles millimeters mils yards atmospheres feet of water kg/sq cm kg/ sq meter pounds/ sq ft pounds/sq in. ~tmospheres

2.540 2.540 x 10 - 2 l.5 78x 10-5 25.40 1,000.0 2.778X 10-2 0.03342 1.133 0.03453 345.3 70.73 0.4912 2.458x 10 - 3

inches of mercury

0.07355

kg/ sq cm

2.540x 10-3

ounces/sq in.

0.5781

po,unds / sq ft

5.204

pounds/ sq in .

0.036 13

ampere (a bsolute)

0.9998

15-9

( TO CONVERT

INTO

international volt international volt international volt

volts (absolute) joules (absolute) joules

1.0003 1.593x 10-19 9.654x 10 4

joules joules joules joules joules joules joules/cm joules/cm joules/cm

J Btu ergs foot-pounds kg-calories kg-meters watt-hr grams dynes joules/meter

9.480x 10- 4 10 7 0.7376 2.389X 10-4 0.1020 2.778X 10- 4 1.020X 10 4 10 7 100.0

joules/cm joules/cm

poundals pounds

kilograms kilograms kilograms kilograms

dynes grams joules/cm joules/meter (newtons) poundals pounds tons (long) tons (short) grams/cu cm

70.93 2.205 9.842x10- 4 1.102X 10- 3 0.001

pounds/cu ft

0.06243

pounds/cu in.

3.613X 10-5

pounds/mil-foot

3.405 x 10- 10

pounds/ft dynes atmospheres feet of water inches of mercury pounds/sq ft pounds/sq in. atmospheres

0.6720 980,665.0 0.9678 32.81 28.96 2,048.0 14.22 9.678X 10-5

feet of water

3.281x10-3

MULTIPLY BY

(ne~tons)

723.3 22.48

K

kilograms kilograms kilograms kilograms kilograms/cu meter kilograms/cu meter kilograms/cu meter kilograms/cu meter kilograms/ meter kilograms/sq cm kilograms/sq cm kilograms/sq cm kilograms/sq cm kilograms/sq cm kilograms/sq cm kilograms/sq meter kilograms/sq meter

15-10

980,665.0 1,000.0 0.09807 9.807

"

...

... ......

TO CONVERT

IN TO

MULTIPLY BY

kilograms/sq meter kilogra ms/sq meter kilograms/sq meter ki lograms/sq mm kilogram-calories kilogram -ca lor ies kilogram -ca lories kilogram-calories kilogram -calo r ies kilogram-calor ies kilogram-ca lories kilogram meters kilogram meters kilogram meters kilogra m meters kilogram meters kilogram meters kilol in es kiloliters kilometers ki lometers kilometers kilometers kilometers kilometers ki lometers kilometers/hr kilometers/ hr kilometers / hr kilometers/ h r kilometers/ hr kilometers / hr kilometers/ hr I sec ki lometers/ hr I sec kilometers/hr I sec kilometers/ hrI sec kilowatts kilowatts kilowatts

inches of mercury

2.896x 10 - 3

pou nds/sq ft

0.2048

pounds/sq in.

l .422x 1 0- 3

kg/sq meter Btu foot-poun ds hp-hr joules kg-meters kilojoules kilowatt-hr Btu ergs foot-pounds joul es kg-ca lor ies kilowatt-hr maxwell s liters centimeters feet inches meters miles millimeters yards ems/sec feet/min feet/sec knots meters/ min miles/ hr cm s/ sec/ sec

10 6 3.968 3,088.0 l.560X 10-3 4, 186.0 426.9 4.186 l.163X 10- 3 9 .294x 10- 3 9.804xl0 7 7.233 9 .804 2.342x 10 - 3 2.723x 10 - 5 1 ,000.0 1,000.0 10 5 3,281.0 3.937 x 10 4 1,000.0 0.6214 10 6 1,094.0 27.78 54.68 0 .9113 0.5396 16.67 0.6214 27 .78

ft/sec/ sec

0.9113

meters/ sec/ sec

0.2 77 8

miles/ hr/sec

0.6214

Btu/min foot-lb/ min foot-lb/ sec

56.92 4.426 x 1 o• 73 7 .6

15-11

( TO CONVERT kilowatts kilowatts kilowatts kilowatt-hr kilowatt-hr kilowatt-hr kilowatt-hr kilowatt-hr kilowatt-hr kilowatt-hr kilowatt-hr kilowatt-hr kilowatt-hr knots knots knots knots knots knots league light year light year lines/sq cm lines/sq in. lines/sq in. lines/sq in. lines/sq in. liters liters liters liters liters liters liters liters liters/min liters/min

INTO horsepower kg-calories/min watts Btu ergs foot-lb gram-calories horsepower-hr joules kg-calories kg-meters pounds of water evaporated from and at 212°F pounds of water raised from 62 ° to 212°F feet/hr kilometers/hr nautical miles/hr statute miles/hr yards/hr feet/sec L miles (approx) miles kilometers gausses gausses webers/sq cm webers/ sq in. webers/sq meter cu cm cu feet cu inches cu meters cu yards gallons (U.S. liq) pints (U.S. liq) quarts (U.S. liq) cu ft/sec gal/sec

MULTIPLY BY

1.341 14.34 1,000.0 3,413.0 3.600x 10 13 2.655x10 6 859,850.0 1.341 3.6X 10 6 860.5 3.671X10 5 3.53 22.75 6,080.0 1.8532 1.0 1.151 2,027.0 1.689 3.0 5.9 x 10 12 9.46091x10 12 1.0 0.1550 1.550x 10-9 10-s l.550x 10-5 1,000.0 0.03531 61.02 0.001 l.308X 10-3 0.2642 2.113 1.057 5.886X 10-4 4.403X 10-3

'-"

l_.I

'-"'

15-12

r TO CONVERT

.....,

...,

maxwells maxwells mega lines megohms megohms meters meters meters meters me~ers

meters meters meters .._ meters/min meters/min meters/min meters/min meters/min meters/min meters/sec meters/sec meters/sec meters/sec meters/sec meters/sec meters/sec/sec meters/sec/sec meters/sec/sec meters/ sec/ sec "...; meter.kilograms meter·kilograms meter.kilograms microfarad micrograms microhms · microhms '-11 microliters miles (nautical) miles (nautical) miles (nautical) miles (nautical) "'-"miles (nautical) miles (statute) miles (statute)

INTO

MULTIPLY BY

M kilolines we be rs maxwells microhms ohms centimeters feet inches kilometers miles (nautical) miles (statute) millimeters yards cm/sec feet/min feet/sec km/hr knots miles/hr feet/min feet/sec kilometers/hr kilometers/min miles/hr miles/min cm/sec/sec ft/sec/sec km/hr/sec miles/hr/sec cm·dynes cm.grams pound.feet farads grams megohms ohms liters feet kilometers meters miles (statute) yards centimeters feet

0.001 10-s 10 6 10 12 10 6 100.0 3.281 39.37 0.001 5.396x 10- 4 6.214X 10-4 1,000.0 1.094 1.667 3.281 0.05468 0.06 0.03238 0.03728 196.8 3.281 3.6 0.06 2.237 0.03728 100.0 3.281 3.6 2.237 9.807x 10 7 10 5 7.233 10- 6 10- 6 10-12 10- 6 10-6 6,080.27 1.853 1,853.0 1.1516 2,027.0 1.609x 10 5 5,280.0

15-13

'

r

I

TO CONVERT

INTO

MULTIPLY BY

miles (statute) miles (statute) miles (statute) miles (statute) miles (statute) miles/hr miles/hr miles/hr miles/hr miles/hr miles/hr miles/hr miles/hr miles/hr /sec miles/hr /sec miles/hr/sec miles/hr/sec miles/min miles/min miles/min miles/min miles/min mil-feet milligrams milligrams/liter m illihen ries milliters millimeters millimeters millimeters millimeters millimeters millimeters millimeters millimeters million gal/day mils mils mils mils mils mils minutes (angles) minutes (angles) minutes (angles) minutes {angles)

inches kilometers meters miles (nautical) yards cm/sec feet/min feet/sec km/hr km/min knots meters/min miles/min cm/sec/sec feet/ sec/ sec km/hr/sec meters/ sec/ sec cm/sec feet/sec km/min knots/min miles/hr cu inches grams parts/million henries liters centimeters feet inches kilometers meters miles mils yards cu ft/sec degrees (angle) centimeters feet inches kilometers yards degrees quadrants radians seconds

6.336x 10 4 1.609 1,609.0 0.8684 1,760.0 44.70 88.0 1.467 1.609 0.02682 0.8684 26.82 0.1667 44.70 1.467 1.609 0.4470 2,682.0 88.0 1.609 0.8684 60.0 9.425x 10-6 0.001 1.0 0.001 0.001 0.1 3.281x10-3 0.03937 l0-6 0.001 6.214x 10-1 39.37 l.094X l0- 3 1.54723 0.05625 2.540x 10- 3 8.333x 10- 5 0.001 2.540 X 10-8 2.778x 10- 5 0.01667 1.852 x 10- 4 2.909X 10- 4 60.0

15-14

~

'-"' '..!

'..I

~

'

'-' C3

TO CONVERT

.... '-

INTO

MULTIPLY BY

0 ohms (international) ohms ohms ounces ounces ounces ounces ounces ounces ounces (fluid) ounces (fluid) ounces (t roy) ounces (troy) ounces/sq in. ounces/sq in.

ohms (absolute)

1.0005

megohms micr ohms drams grams pounds ounces (troy) tons (long) tons (metric) cu inches liters grams pounds (t roy) dynes/ sq cm pounds/sq in.

lo- 6 l 06 16.0 28.349527 0.0625 0.9115 2 .790x 10- 5 2.835 X 10-5 1.805 0 .02957 31.103481 0.08333 4309 .0 0.0625

p

....

parts/million parts/ million parts/ million pints (dry) pints (liq) pints (liq) pints (liq) pin ts (liq) pints (liq) pints ( liq) pints (liq) pints (liq) pounds (avoirdupois) poundals poundals poundals poundals pounda ls pounda Is pounds pounds pounds pounds pounds

grains/ U.S. gal grains/ Imp . gal pounds /million gal cu inches cu cm cu feet cu inches cu meters cu yards gallons liters quarts (liq) ounces (troy)

0.0584 0.07016 8.345 33.60 473.2 0.01671 28.87 4 .732x10- 4 6.189x 10- 4 0.125 0.4732 0.5 14.5833

dynes grams joules/ cm joules/meter (newtons) kilograms pounds drams dynes grains grams joul es / cm

1 3,826.0 14.10 1.383 x 10- 3 0.1383 0.01410 0.03108 256.0 44.4823x 10 4 7,000.0 453 .5924 0.04448

15-1 5

( TO CONVERT pounds pounds pounds pounds pounds pounds pounds pounds (troy) pounds (troy) pounds (troy) pounds (troy) pounds (troy) pounds (troy) pounds .(troy) pounds of water pounds of water pounds of water pounds of water I min pound-feet pound-feet pound-feet pounds/ cu ft pounds/ cu ft pounds/cu ft pounds/cu ft pounds/cu in. pounds/cu in. pounds/cu in. pounds/cu in. pounds/ft pounds/in. pounds/mil-foot pounds/sq ft pounds/sq ft pounds/sq ft pounds/sq ft pounds/sq ft pounds/sq in. pounds/sq in. pounds/sq in. pounds/sq in. pounds/sq in.

15-16

INTO

MULTIPLY BY

joules/meter (newtons) kilograms ounces ounces (troy) poundals pounds (troy) tons (short) grams ounces (avdp.) ounces (troy) pounds (avdp.) tons (long) tons (metric) tons (short) cu feet cu inches gallons cu ft/sec

0.4536 16.0 14.5833 32.17 1.21528 0.0005 373.24177 13.1657 12.0 0.822857 3.6735 x 10- 4 3.7324x 10- 4 4.1143x 10- 4 0.01602 27.68 0.1198 2.670x 10- 4

cm-dynes cm-grams meter-kg grams/cu cm kg/cu meter pounds/cu in. pounds/mil-foot gm/cu cm kg/cu meter pounds/cu ft pounds/mil-foot kg/meter gm/cm gm/cu cm atmospheres feet of water inches of mercury kg/sq meter pounds/sq in. atmospheres feet of water inches of mercury kg/sq meter pounds/sq ft

1.356x10 7 13,825.0 0.1383 0.01602 16.02 5.787x10- 4 5.456 x 10- 9 27.68 2.768x 10 4 1,728.0 9.425 x 10- 5 1.488 178.6 2.306x10 6 4.725x 10-4 0.01602 0.01414 4.882 6.944 x 10- 3 0.06804 2.307 2.036 703.1 144.0

4.448

'W

'-'

iW

TO CONVERT

.... """"'

....

.......

INTO

M U LTIPLY BY

Q

90.0 5,400.0 1.571 3.24x10 5 67.20 946.4 0.03342 57.75 9.464x 10 - • l.238 x10 - 3 0.25 0.9463

quadrants (angle) quad rants (angle) quadrants (angle) quadrants (a ngle) quarts (dry) quarts (liq) quarts ( liq ) quarts (l iq) quarts ( liq ) quarts (liq) quarts (liq) quarts (liq)

degrees minutes radians seconds cu inches cu cm cu feet cu inches cu meters cu yards gallons liters

rad ians radians radians rad ia ns radians/sec rad ia ns/ sec radians/ sec radians /sec/sec radians/sec/sec radians/ sec/ sec revolutions revolution s revolutions revolut ions/min revolutions / min revolutions/m in revolutions/ min / min revolutions/ min/ min revolutions/ min / min revolutions/ sec revolutions/ sec revolutions/sec r evolutions/ sec/ sec revolutions/sec / sec revel ution s/ sec/ sec

degrees minutes quadrants seconds d egrees/sec revolutions/mi n revolutions/sec rev/ min / min rev/min/sec rev/ sec/ sec degrees quadrants rad ians degrees/ sec radians/sec rev / sec radians/sec/ sec

57 .30 3,438.0 0.6366 2.063x 10 5 57.30 9.549 0.1592 573.0 9.549 0.1592 360.0 4.0 6.283 6.0 0. 1 047 0.01667 l.745x 10 - 3

rev/min/sec

0.0 1667

rev /sec/sec

2.778X 10 - 4

degrees/ sec rad ians/sec rev/min radians/sec/sec

360.0 6.283 60.0 6.283

rev/mi n/ min

3,600.0

rev/ min/sec

60.0

R

15- 17

~ INTO

TO CONVERT

MULTIPLY BY

s seconds (angle) seconds (angle) seconds (angle) seconds (angle) slug slug square centimeters square centimeters square centimeters square centimeters square centimeters square centimeters square centimeters square feet square feet square feet square feet square feet square feet square feet square feet square inches square inches square inches square inches square inches square inches square kilometers square kilometers square kilometers square kilometers square kilometers square kilometers square kilometers square meters square meters square meters

15-18

degrees minutes quadrants radians kilogram pounds circular mils

2.778X 10- 4 0.01667 3.087x10- 5 4.848x 10- 5 14.59 32.17 l.973x 10 5

sq feet

1.076x10-3

sq inches

0.1550

sq

0.0001

m~ters

sq miles

3.861x10- 11

sq millimeters

100.0

sq yards

1.196x 10- 4

acres circular mils sq cm sq inches sq meters sq miles sq millimeters sq yards circular mils sq cm sq feet sq millimeters sq mils sq yards acres sq cm sq ft sq inches sq meters sq miles sq yards acres sq ems sq feet

2.296x 10- 5 l.833x 108 929.0 144.0 0.09290 3.587x10- 8 9.290x 10 4 0.1111 1.273 x 10 6 6.452 6.944 x 10-3 645.2 10 6 7.716X 10-4 247.1 1010 10.76x 106 l.550x 109 10 6 0.3861 1.196X 10 6 2.471x10-4 10 4 10.76

~

'-"

TO CONVERT

INTO

MULTIPLY BY

square meters square meters square meters square meters sq uare miles squa re miles square miles sq uare miles square miles squa re millimeters square millimeters square millimeters sq uare millimeter s square mils square mils square mils square yards square yards square yards square yards square yards square yards square yards

sq inches sq miles sq millimeters sq yards acres sq feet sq km sq meters sq yards circular mils sq cm sq feet sq inches circular mils Sq CrTI sq inches acres sq cm sq feet sq inches sq meters sq miles sq millimeters

tern peratu re c °C) +273 temperature (°C)+ l7.78 temperature ( ° F) + 460 temperature (°F)-32 tons ( lon g) tons (long) tons (long) tons (metric) tons ( metric) tons (short) tons (short) tons (s hort) tons (short) tons (short) tons (short) tons (short) tons (short) sq ft

absolute tempera · tu re ( °C) temperature ( ° F)

1.0

absolute temperature(°F) temperature ( • C)

1.0 5/ 9

kilograms pounds tons (short) kilograms pounds kilograms ounces oun ces (troy) pounds pounds (troy) tons ( long) tons (metric) kg/ sq meter

1,016.0 2,240.0 1.120 1,000.0 2 ,205.0 907. 1848 32,000.0 29 , 166.66 2,000 .0 2, 430.56 0.89287 0.9078 9.765.0

1,55 0.0 3.861x10- 7 106 1.196 640.0 27.88xl0 6 2.590 2.590x 106 3.098 x 106 1,973.0 0.01 1.076x 10- 5 1. 550x10- 3 1.273 6.452 x 10-6 10-6

2.066X 10- • 8 ,36 1.0 9.0 1 ,296.0 0.8361 3.288x 10- 1 8.36lx10 5

T

....,

1.8

15- 19

( TO CONVERT tons (short)/ sq ft tons of water I 24 hr tons of water I 24 hr tons of water I 24 hr

INTO

MULTIPLY BY

pounds/sq in.

2,000.0

pounds of water I hr gallons/min

83.333

cu ft/hr

1.3349

0.16643

w watts watts watts watts watts watts watts watts watts watts (absolute) watts (absolute) watt-hours watt-hours watt-hours watt-hours watt-hours watt-hours watt-hours watt-hours watts (International) we be rs we be rs webers/sq in. webers/ sq in. webers/sq in. webers/sq in. webers/sq meter we be rs/ sq meter webers/sq meter webers/sq meter

Btu/hr Btu/min ergs/sec foot-lb/min foot-lb/sec horsepower horsepower (metric) kg-calories/min kilowatts Btu (mean)/min joules/sec Btu ergs foot-pounds gram-calories horsepower-hr kilogram-calories kilogram·meters kilowatt-hr watts (absolute)

3.4129 0.05688 107.0 44.27 0.7378 1.341xi0- 3 l.360X 10- 3

maxwells kilolines gausses lines/sq in. we be rs/ sq cm webers/sq meter gausses lines/sq in. webers/ sq cm we be rs/ sq in.

10 8 10 5 l.550x 10 7 10 8 0.1550 1,550.0 10 4 6.452x10 4

0.01433 0.001 0.056884 1.0 3.413 3.60X 10 10 2,656.0 859.85 1.341x10-3 0.8605 367.2 0.001 1.0002

'-'

\_.;

10-4

6.452x10- 4

"wl

15-20

TO CONVERT

INTO

MULTIPLY BY

y 'W'

centimeters kilometers meters miles ( nautical) miles (statute) millimeters

yards yards yards yards yards yards

91.44 9. 144X 10-• 0.9144 4.934x10 - • 5.682 x lo-• 914.4

Metric Unit Prefixes Prefixes tera· giga· mega· myria· kilo· hekto· deka ·

Multiples 1012

Prefixes deci·

10 9 10 6

centi· milli·

lo•

micro· nanopico·

10 3 10 2 10

Multiples 10- 1 10- 2

10 - 3 10 - 6 10-9 10-12

15-21

Centigrade-Fahrenheit Conversion Table °F=9/5 °C+32=1.8 (°C+l7.8) °C=5/9 (°F-32) C._F

-62.2 -56.7 -51.1 -45.6 -40.0 -34.4 -31.7 -28.9 -26.1 -23.3 -20.6 -17.8 -15.0 -12.2 - 9.4 - 6.7 - 3.9

-

-

-

-

-

-

C~F

C-.F

-112.0 - 94.0 76.0 58.0

43.3 46.1 48.9 51.7

110 115 120 125

230.0 239.0 248.0 257.0

-

40.0 22.0 13.0 4.0

54.4 57.2 60.0 62.8 65.6

130 135 140 145 150

266.0 275.0 284.0 293.0 302.0

+

5.0 14.0 23.0 32.0

68.3 71.1 73.9 76.7

155 160 165 170

311.0 320.0 329.0 338.0

79.4 82.2 85.0 87.8

175 180 185 190

347.0 356.0 365.0 374.0

195 200 205 210

383.0 392.0 401.0 410.0

80 70 60 50

-

40 30 25 20

-

15 10 5 0

C_.F

5 10 15 20 25

41.0 50.0 59.0 68.0 77.0

1.1 1.7 4.4 7.2

30 35 40 . 45

86.0 95.0 113.0

90.6 93.3 96.1 98.9

10.0 12.8 15.6 18.3

50 55 60 65

122.0 131.0 140.0 149.0

101.7 104.4 107.2 110.0

215 220 225 230

419.0 428.0 437.0 446.0

21.l 23.9 26.7 29.4

70 75 80 85

158.0 167.0 176.0 185.0

112.8 115.6 118.3 121.1

235 240 245 250

455.0 464.0 473.0 482.0

32.2 35.0 37.8 40.6

90 95 100 105

194.0 203.0 212.0 221.0

126.7 132.2 137.8 143.3

260 270 280 290

500.0 518.0 536.0 554.0

15-22

~04.0

Centigrade-Fahrenheit Conversion Table-Continued °F=9/ 5 °C+32=1.8 (°C+l7.8) "C=5/9 (" F- 32) C-+--F

C-...F

C.-F C-.F

148.9 154.4 160.0 165.6

300 310 320 330

572.0 590.0 608.0 626.0

265.6 271.1 276.7 282.2

510 520 530 540

950.0 968.0 986.0 1004 .0

171.1 176.7 182.2 187.8

340 350 360 370

644.0 662.0 680.0 698.0

287.8 293.3 298.9 304.4

550 560 570 580

1022.0 1040.0 1058.0 1076.0

193.3 198.9 20 4.4 210.0 215.6

380 390 400 410 420

7 16.0 734.0 752.0 770.0 788.0

310.0 315.6 326.7 337.8

590 600 620 640

1090.0 1112.0 1148.0 1184.0

221.1 226.7 232.2 237.8

430 440 450 460

806.0 824.0 842.0 860.0

348.9 360.0 371.l 382.2

660 680 700 720

1 220.0 1 256.0 1292.0 1328.0

243.3 248.9 254.4 260.0

470 480 490 500

878.0 896.0 914.0 932.0

393.3 404.4 415.6 426.7 437.8

740 760 780 800 820

1364.0 1400.0 1436.0 1472 .0 1508.0

15-23

NUMBER SYSTEMS Decimal

Octal

Base or Radix

10

8

2

Total Symbols

10

8

2

Counting

l

0 1 2 3

0 1 2

10

3

4

4 5 6

!!

100 101 110

10 11 12 13 14 15 16 17 20 21 22 23 24 25

1000 1001 1010 1011 1100 1101 1110 1111 10000 10001 10010 10011 10100 10101

5 6 7 8 ~

10 11 12 13 14 15 16 17 18 19 20 21

15-24

Binary

z

0

.!

ill

VARIOUS RADICES (Radix- Base)

10 20 30 40 50 11 12 13 14 15 16 17 18 19 29 39 49 59 20 30 Radix 2 1 21 31 Radix 3 2 12 22 32 Radix 4 3 13 23 33 4 14 24 34 Radix 6 5 15 25 35 6 16 26 36 7 17 27 37

0 1 2 3 4 5 6 7 8 9

1_l1J

....

90 100

99 40 41 42 43 44 45 46 47

50 51 52 53 54 55 56 57

Radix 2 00 01

io

!..!!

100 101

00 10 20 01 11 21 02 12 210 220 21 1 221 212 2221

w

110

!.!..!I

1000 1001

1010 10111

Radix 3 100 110 120 200 101 111 121 201 102 112 122 1 202 1000 1010 10 20 1001 1011 1021 1002 1012 10221 Radi x 5

00 01 02 03 04

10 11 12 13 14

20 21 22 23 24

30 31 32 33 34

40 41 42 43

~

100 101 102 103 104

110 111 112 113 114 15-25

ANALYSIS OF NUMBERS Decimal

982.4 9 = 9

2

x 10 10 = 9 x 100 = 900

1 8=8X 10 10

=BX 10 = -80

0 2 = 2 x 10 10 =2X

1 = ····2

-982

4 = 4 x 10-l = 4 x 1/10 = ·····-.4 10· -982.4 Octal

674.2 6 = 6 7

=7

x

8 2 = 6 8

x

100

= 600

1 = 7 8

x

10

= --70

=4X

1

= .... 4

x8

4=4X80 8

674 -1 2 = 2 x 8 8 = 2 x 1/10 = ····-.2

674.2

. 15-26

Binary

10110.01 4

1

=

0

=0 x

2

3 - 0 2 -

1

=1 x

2

2 2

=1x

100

= ----100

1

=1 x

2

1 2

=1x

10

= ··----10

0

=0 x

2

0 2

=0 x

1

1

x 2

2

=

1

x 10000 = 10000 x 1000

= -·0000

=

__.______ o

I

10110 0

=0

1

=1x

x 2

-1 2

=0

-2

=1 x

2 2

x 1/ 10 1/ 100

= ··········.O = ----------.01 10 110.01

C4

15-27

'

N CIO

I

....UI

(

Large base

Small base

,'

Fractiona I

Large base

Small base

(

Integral

Small base

Large base

{

Fractional

Integral

Small base

Large base

Number

To

From

Systems

(

{

Divide entry number by small base and record remainder. First digit is LSD and last digit is MSD. (Read up.) Multiply entire number by small base and record remainder to left of radix point. First digit is MSD. (Read down.) Multiply from left by small base and add next digit. The last step is add. Last number is answer. Divide each digit from the right by small base. Add next digit. Last step divide. Last quotient is answer.

Instruction

GENERAL RULES FOR NUMBER SYSTEM CONVERSION

(

Large base

Large base

Large base

Large base

Arithmetic done in

~

'

EXAMPLES OF NUMBER CONVERSIONS Decimal to Octal

8

•

. 1~;:10 ,= 5348 8

5 0

3 5

2

2

0 0

2

1

0 1 1 1 1

.531 0

1:

= .4 17 8

.4510

8

2

.24 8

.90 2

.92 8

r

.80 2

.36

.60

Octa l to Decimal

= 19010

x:7Ll68 16

Binary to Decimal 110

x~~

...±l...

+l

23 x8 184 ...±..§. 190

3 x2 6 +O Answer

.5 ;J

.648

= .0 112

= .812510

6

= 6 10

An swer

= .8 12510

8 14.00

.8 125 8 16.5

15-29

DECIMAL TO OCTAL CONVERSION Number Less Than 1 1. Multiply number of s 1 . 0 2. The integral portion of the ·product is the MSD of the decimal number. 3. The fractional portion becomes the multiplicand for successive· multiplication. 4. Continue until sufficient places have been formed. Convert .53 to an octal number. Step 1

.53

8 4.24 Step 3

4 MSD Step 2

.24

8 1.92 .92

8 7.36 Octal Number .417

15-30

7

~

r DECIMAL TO BINARY CONVERSION Numbers Less Than 1 1. Multiply the decimal number by 2. 2. The integral portion of the product becomes the MSB. 3. The fractional portion of the product becomes the multiplicand for the next operation. 4. Continue until sufficient places have been formed . .9125 2 1.8250 1 MSB .8250 2 1.6500 .6500 2 1.3000 .3000 2 .6000

Binary .l l lO number

1

0 LSB

OCTAL TO DECIMAL CONVERSION Numbers Less Than 1 1. Divide the rightmost digit by 8

10

.

2. Add th.e next digit to the quotient. 3. last step, divide. 4. last quotient is the answer. Convert .64

8

to a decimal number.

Decimal number

C4

.8125

15-31

r Bl NARY TO DECIMAL CONVERSION 1. Use positional notation to determine the weight of each digit. 2. Add a II values. Convert 1100.1101 toa decimal number. 1101

1100

wtx2° OX2 2 1X2

1X2

0

11itx~-4

.0000

4

1X2- 2

.2500

0

1

3

8

.0625

3

OX2

1X2- l

.5000

12

.8125

Decimal number 12.8125

OCTAL TO BINARY CONVERSION 1. Mentally convert each octal digit to three binary digits.

5

2

I

010

3

7

\

\

I

101

011

111

BINARY TO OCTAL CONVERSION 1. Group the binary number in threes from the binary point. 2. Mentally convert each group to an octal digit. 0 1 0 1 0

0 1 1 1 1 1

010

101

011

111

2

5

3

7

Use positional values of binary numbers for mental conversion.

0

0

0

+ + + 4

"-32

2

1

C4

DECIMAL TO OCTAL CONVERSION Number Greater Than 1 1. Divide decimal number by 8

10

.

2 . Remai nder is LSD. 3. Div ide quot ient (of step 1 ) by 8

10

.

4. 2nd remainder is 2nd digit. 5. Continue division unti l quotient cannot be divided again. 6. The last r ema in der is the MSD. Convert 348 to an octal number. Stop t Step 3

8

8

Step 5

IH!_ 43

8 5 0

4 LSD

Step 2

3

Step 4

5 MSD

Step 6

Octal number - 534

DECIMAL TO BINARY CONVERSION Numbers Greater Than 1

1. 2. 3. 4. 5.

Divide the decimal num ber by 2. Remainder is LSB. Quotient becomes dividend for next operation . Continue until the number can no longer be divided. The last r ema inder is the MSB.

2 22 ~1!7 2 2

0 LSB

0

3 1 0

Bina ry numbe r 1 11 00 1

1 MSB

15-33

r OCTAL TO DECIMAL CONVERSION Numbers Greater Than 1 1. Multiply the MSD of the octal number by 8

10

2. Add the next significant digit to the product. 3. Multiply the sum by 8

10

.

4. The last step will be add. 5. The last sum will be the answer. Convert 276

8

to decimal number.

xl:~s +7j 23 x 8 184

+6 190

15-34

Decimal number

190

.

If a warhead malfunction E07 or adapter M06 is displayed on the IRI, the following procedures will be followed: 1. Stop all operations on the warhead section, immediately remove electrical power. 2. Wait 30 minutes before performing any operation on warhead section. 3. After 30 Minut es, if applicable, recapture the missile 4. Remove the warhead section from the the guidance section. 5. Test the warhead section with the 4127 A test set. Checking to iasure that the ST-120 is caged 8W2J2 Pins W to X continuity = Caged EMERGENCY INTERRUPT M04 G&C, MOS ADPT, E03 SAF REL-G&C, E04 ADPT, EO~ S&G-G&C MNDIST, E06 ADPT, 547 SAF REl-MNDST G&C IN CONTADIBR 25W9J9 D (-) 25W7J7 36 (+) XlOK Infinity :r 25W9J9 D (+) 25W7J7 36 (-) II II 25Wl 0Jl0 57 25Wl 0Jl0 27 " X16K ~ 10 ohms 25W9J9 D 25W7J7 30 II '"7 11 II 25Wl0Jl0 38 25WlOJ10 56 25W9J9 D 25W7J7 10 Xl <..10 ohms II 25W9J9 F 25W7J7 9 <. " II <... II " 25H9J9 D 25Wl0Jl0 26 II

G&C OUT OF CONTAINER 8W4J4 N (+) 8W4J4 n (-) 8W4J4 n (+) --SW4J4 N (-) 8 W20J2 KK 8W20J2 v 8W4J4 j 8W4J4 N

XlOK Infinity II

:1

"

!I

XlG 710 ohms

r

8W20J2 cc 8W4g4 N 8W4J4 F 8W4J4 N

8W29J2 8W4J4 8W4J4 8W20J2

JJ XlO '> 10 ohms Xl .( tilt " "11 J " < K

u

n

<

n

'

n

'W

Pershing 1a Field Service Data Notebook

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