FOR ER9iATA

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LVM ,

-E Y -. . N O .. . - - - - -.sacy. PAG

SM . . REViSIONS

SYM DESCRIPTION DATE APPROVED

A In"" fo 4 6-1763 D. b"

AU"M IMam 4.0 =a 5.0 to Ow Aovmut.,

3 tI4 YSIM S 3ho 3%,369 No A39,3 ,.Ok,l~ 724-7-61 D.BrmoAf

C Revised Pages 2, 3, 4 .- 16-63 P. Branden

Added Pager 4.1, 52, 53, 54, 55, 56, 5T, 58, 59, 60, 61,62, 63, 64, 65, 66, 67, 68, 69, 70, 71, 72,73, 74, 75, 76,

D Revised Pages 2, 3, 4, 4.1, 6, 52, 53, 54, 55, 61, 6, 65, ]0 16-63 D. Brenden66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76.

Added Pages 2.1, 4.2, 77, 78T9, , 81, 82, 83,.E4, •5, t0,V-

86, 87, 88, 89, 90, 91, 9-, 95, 94 95, 96,97, 98, 99, 100, 101, 102, 103, 104 , 105,

986, 107, 108, 1 12, 113, 114,

115, 116, 117, u18, 119, 120, 121, 122, 123,124, 125, 126, 127, 128, 129, 130, 131, 132,13-1, 134, 135, 136, 13"T, 138, 139.

I Revised Pages 2, 2.1, 3, 4.2, .14, 115, n16, 11T, 118, 119, 1-18-63 D. Brendenla), L2J, 11.3

Addd F&9es 140, 141L, .142, 14i3, 144, 145, 146, 14T, 148, '149, 150, 151, 152, 153, 154, 155.

F Revised Pages 2, 2.1, 3, 4.2, 122, 123, 124, 125, 126, 2-18-6- D. Broaden127, 128, 129, 130

Added Pages 156, 15r, 158, 159, 160, 161, 162, 163, 164,165, 166, 167, 168, 169, 170, 171, 172, 173,174, 187,7, 176, iTT, 178, 1y, 18o, 181, 182,

4.3, 18~3, L8&s, 185, 186, 18T, 188, 189., 190, 191. _____

SMi. PAW(

I. TABEL OF CONTUMT (Cont.)

PAE

13.0 CTIII _&vO!. mm),13.1 DIS SSIO-N 12213.2 WEIGf AND BAIMCE SC WARY 12313. -3 MS3SLE 8NCTION MWA- Y MHEMK LISTL, 12613.4 SEMOIJ 39 DATA 12713. 5 ENGINEERING CHA.M¶E PPOP08A.L SUMM4ARY 130

14.o C SECTIO, SIN oooo6

14.1 DISCUSSION 13/14.2 WEIM AND BALANCE SLM4ARY 13214. j MISSILE SECTION SUhAR C=K LISTS 13514.4 SECTIONK 39 rATA 13ý614. 5 NGDIE~nfa CHAfNGE PfOPOAL SI4MAnY 139

15.0 TLaI SEMON, SIN 0000041

15.1 DIM=OffI 14L6"

15.2 WEIGT AND WALANCE SWNiR 14115.3 MIss= "mcm" alo Cf LISTS 144i15-.- sMT 39 DATA 15215.5 ''T~N ! ANOE PROPOSAL 8U)4A.FY 255

16.o CTII aSCIO, s/N 0oooo048

16.1 DI8CUSSIO 15616.2 WIXOM AND BALANCE SUMMARY 19616.3 MISSILE SECTI(CN SnW4ARY CHECK LISTS 16916.4 SEcTIM 39 DATA 16116.5 1 EEMN CHANGE PROP35AL StI4RY ThL

17.0 cmL 0UCimM. SIN 0000049

17.1 D$CUSeIx(s 16,17.2 WEIV AND BALANCE UWLAM 16617.3 ISSILE sEMC O m( Y LISTS 16017. SECTIK 39 DATA 17I17. 5 rZnl CHAME PROPOSAL K m V

18.0 crim ALMON" I/N o00(A)5

18.2 WIM AND BALANCE 5WA~ff 17518.3 )(MILE SEMCTI ML)ARY M=EC LISTS 17818.4 S=W3 M1T91.8.5 CHNEPwmSo m182

V)~~o P SSV. RE 5.,4-

SaCT. IPAUK4

TA= OF CONTWI! (C-ant.)

PAGE

19.0 RoomX S~~X~ /N 0oooLX)5

19.1 DISCUSSION~ 18319.2 WZIXIT AND WAIACE MJWAO 184

19. 3 MISSILE SEICTIO M.34P CEMi LISTS 187

19.4 SiEOTIOMN 3 DATA 188

19.5 GI~N CHANG ?)pwGA 191

Ii)w go ftePO EV. t4

-75 ýu y e-34-

Ca=U SwCaox, SIN 0000045

13.1 This section of the docuenlt describes the date changes created byconverting a production line Minuteman missile into a CTL missile.The mass data reported herein reflect the predicted net changes to beapplied to the total missile mass properties when this CTLI sectionand the related downstage ecoponents are installed on a aissile. Asupplemental report (see reference I.i.6) will be issued at VandenbergAir Force Bease when this 0=LI sectio)n is actually used on a missile.This supplemental report viii reflect the actual data gathered onbase during tAe installation and will thus sulacfrsede parts of thisreport. However, past experience hais ihovn that the changes betweenthese tv..- re•prts will be slight.

The data on the following pages consist of weight and lalance sumnariescheck lists, and ECP's lists applicable to this installation. Page 123sumarizes the complete installation mass properties and consists ofdata from page 124 (average mass pr perties of downstage crmponents),page 125 (predicted sealant changes), and page 1.2 (actual weight ofCMLI section S/N 0000045). In additLin, page i16 presents suiay checklists by production section as backup data for page 12i. Page 130 liststhe engineering change proposals incorporated on the components usedfor this Installation.

All data reported in this section (,f the document reflect the use ofa linear shaped charge destruct system on the first atage engine permP 116.

Aerojet weights used in this report reflect the data transmitted toBoeing by Aerojet document 0l62-l-DP-NmID-i, "IN minal Mass Properti esand Dispersions for Minuteman CTLI/AOD" dated January 28, 1963.

Average values have been used for all boeing items other than theCMLI section which is an actual weight.

The following drawings arm incorporated in the above section:

10-2D0942, Battery Instl., Rev. H 6-10-63.21-52900, Missile Znstl., Rev. K 9-19-63.25-25406, MS 5-&6 Instl., DCN J 9-13-63.25-26878, Cable Assy., DO J 9-3-63.25-37060, Conduit Assy., DCO B 9-10-63, ADON S-20 1O-22-63.25-37236, Ixntl. xit, DCw c 6-28-63.25-37237, Conduit Supt. Set, DON A 5-10-63.25-37501, 39 Sect. Izstl., =X C 11-5-63.29-M 32T, Timer Instl., DMN D 6-24-63, ADeN S-6 9-5-63.

"I)S a"O Rev, &/OR

UfV S I- Ao&O.~OUA

13.2 W= & ShLANCI 8WAR RPOT OTOM. amL X7RFOT 9

~~/ L 000 DATZ _ _ _ _ _ _

cdv OA ,4TRO RVT INERTIAH, DESCRIPTION DATA malf 1froTA -ETRO RVT swa Wn'm -3

-- a CR -. - -I; - -,I

A. 3CTL Sgci9A~ I~T~T 9~L1~ _.X4no .002-

Silo

94 Aero

2 . 5 1j(wdSileo __ -

171j ___ Base

SI~ __

274 1 1eo

2 ~~Base -11

m- -J-utjiZotiox - --

_1. 12S.2

3x Aero - - - ---- __- _ _ -

43 -- Base --- --- -

2.~ ....... - .---

~ ____ --.- - - ___!M-..

-A-IL-.

W-1 *30

-~~~c 00", 19~1 IPG 3

1.3.2 W!!(N & MZANCE VaWU M RPOT O(AV!RAG~ ~ ~~duur.1~)DATE ______

DATA OT¶.. CEN1TER OF ORAY ITT SLUG FT2xlo-~3

09C*PIf DAT -SGH - .... bL T iI7 W 1__(JL B) __) wa -.- . V_

v 3 *K 111. _- - - - -- ____

9 9TWA~.. _____

714_ -q 68.1 118.T~ 11 .0 0 0_

~.L~ .Pt~t.~9l _ Base - __

151 4 y ter3~k tali_ _13.7A _Q. 0

16 (AfK -___ _

23 .0t)

25_ __91_ _42 __

35.E~aa._ _~-

T3.i ~ 2z. 6j~ 11 1 25. 0 0138 •Aft) ~Silo _______

lp-i 25.9 115.8- 11.7- J. 2- 0 _ _-

4-2- SAa. ----

-P -0

-~~ ~~~ VOLer. --- ---

13.2 30 5-&2 CJMG =TAIJAP AT WZORT NO.SAIR FOSCE MBP• DATS

DL~~CUPTION ?4CENER OF GRAVITY SU Ti-

Int~~r~taBe %Ls :7.-- jAero __

9-1~ 4 BAer _ _7K q- _ 71-77-6

8102

-•. . . .. ... . . ± A L 2 I _ -... - -_

1_ . ,.H.2_ . l- i ...

2?.4 719-717111 167ZI_

____ sio. ..7___-___7.__ ._ "_ _ . ......_ ___ ..~.....

-- _ --. _e ___ ... . . ,

16 _ __ ......... . L.Ze o ... ..... . ...... .. .. . .. ....... .. .. ..

28 ~ o. BAse.

6 1- Silo

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2~M r __ _ A 11 3,

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13.5 CRANSG PROPOSAL (act) DI1CMWPOMTIONAPPLIANS ToOW C =CN B3 6ZI /N W=O45 AMD DI5TALATIN KIET

The following NMI'# have not been incorporated into "Model SpecificatioA,Trainer-Tet Group, Oudded Misile, (S-133-i006-o-I)".

(W-l33•&-O-) CWGo11OGR KcATIP

~ IN THIS HOW54 Potting & Banding Deletions for All ) No*

Veandmberg Air Force Base Missiles

o06 Revisiom to CTLI Unbilical bracket- I Negl. YesSection 49

620 Addition of Static Dissipatora Neg!. Yeson 47 Section & Section 49 .

635 'PCX R/F Section Digital Data 3 Negl. YesPregremwer

639 Prevent Interference of TAnear 3 Negl. YesShape Charge with Cable Strap

657 Revision of Ordnance Supports in 2 Negl. YesIrnterstage 2-3

660 Wing Ina U&C Section & Raceway 3 Negi. YesRevisions~

Xba properties of other applicable ECP's have been

incorporated

* MP 540 transfers the responsibility fir sealing the raceway covers from

Plant 77 to Vandenberg. However, the weight is still considered part ofthe operational missile and is not included in this report.

as 00 ma00REV. Sf42

REV SYM~......

o=L swumC, s/N 0000048

16.1 This section of the d4oeiient decribes the data changes created byconverting a production line Xftjutinn missile into a CTL missile.The mass data reported herein reflect the predicted net changes to beapplied to the total missile smo pruperties when this (M sectionand the related downstage epooents are installed on a misslie. Asupplemental report (see reference 1.1.6) will be issued at VandenbergAir Force ease when this O=LI section is actually used on a missile.This supplemental report will reflect the actual data gathered onbase during the installation and will thus supercede parts of thisreport. However, past experience has shown that the changes betweenthese two reports will be slight.

The data on the following pages consists of weight and balance susmariescheck lists, and ECP's lists applicable to this installation. Page 157suonarizes the complete installation mass properties and consists ofdata frcm page 158. (average mass properties of downstage components),page 159 (predicted sealant changes), and page 163 (actual weight ofMU section 8/N 0000048). In addition, page 160 presents summary checklists by production section as backup data for page 158. Page 164 liststhe engineering change proposals incorporated on the components usedfor this installation.

All data reported in this section of the document reflect the use ofa linear shaped charge destruct system on the first stage engine perExT 116.

Aerojet weights used in this report reflect the data transmitted toB-eing by Aerojet document 0162-OIDR-SPD-1, "Nominal Mass Propertiesand Dispersions for Minuteman CTLI/AODs" dated January 28, 1963.

Average values have been used for all Boeing itemns other than theCTLI section which is an actual weight.

The following drawings are incorporated in the above section:

10-20942, Battery Lnwtl., Rev. H 6-10-63.21-52900, Missile Irstl., Rev. K 9-19-63.25-254o6, W 5-62 inatl., Dcx j 9-13-63.25-26878, Cable Assy., DCX J 9-3-63.25-37060, Conduit Assy., DoN B 9-10-63, ADCN S-20 10-22-63.25-37236, Instl. Kit, DO C 6-28-63.25-3723T, Conduit Supt. Set, DCX A 5-10-63.25-3T501, 39 Sect. Instl., DCK C U-5-63.29-232T7, Timer Instl., DON D 6-24-63, AMON S-6 9-5-63.

us a" MO Rev. eon 418

Ms~v SYG4 M I a-i 3

16.2 W=W IUAMM 8SM 333 N

OI=L WMAI 8 N11QOOh.8 DAlI_______ ______BIM TOTAL CENTER OF GRAVITY IArrl-DESCRIPTION DAT'A '' MOXroIi

9---I__ __ ___ - _• _ __ _ _ _ _~1

-f 4.._ . +_.____ _____--___-

12 .- k _L t . ........ _t_ _ _,_

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-,• ! 1 ...... . . . _ _ _

16 Agro1117 11 .0

. .___ B�at.._0._

9iF_._k.__• o.t eL_ ._A _r__

-17 ks - --

I..._---._ -_ _ _

~ 1 t2~iitr iu .~____ - T X ~ T I -I i iii

4 . i ---_• Base

me 1-" 25.2 _- .0. 12 .... .

•__ _ + Y2-Q -1 --7 n -7-

"________- E o. .. . _ ,,, - - - -iil

511 -16--,

iz-J L - _ _ - -- " -7 -

I A*- -'r"'+ +'r~k ': .• ' • +'=•'• 4 " "+"" --ratcm . .. . W'sr .1 IEtatlLoa+'+ ' ''"r ,+ .. +- "+-

r -+ ."+<r,..+*+•':. ..... •',.+ + ' ++,+• :• • " ."_ .-+ +5.iO.... "8r £ P .. . . qW . ....... 4 +4+ •, ;+ 1 .]+ + : : .: + .+ .. . .. . : . .. . . .i . + + + / . . ,, + i + . ' . + +" - '+ + i . . .. .: . :,l+ i . .L. . .." . ... . . .' . . .

16.2 wx & MIAWZU.K AX vi a REPORT NO._________(AVUMG WIMR CMVM DATE ______

T - m

5,1 _94 11. -0 -.0LI! !~

Aera o

__________ 0a.0

Aoro _ ~-

20 ____ JrJ 10 0 A

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3 JVO

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16.2 3W 5.62 MOMU MMUMtL AT RtWPORT PO.A~~~ ~~ DATI _______

TOTALINERT IA- fI Zvry-daCIPI!On DAA V Wr¶)aL C04TER Of GRAVITY SIM FTTx1O-

Leh - --SI-

7 R& --- __ A £5V.2Q

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11.2 & RI 1AIOR3WMREPORTY NO.YTAL MUZ M MUTIO,~N

DB8CRPPIO DATA VIG1TOVXTA CENTER OF GRAY IT SLUG FTxiO-I- VERYT __0U PTTCR

.Silo

--- --------

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-4-4 -__ _ -Si]-4 3 9.-F 1.

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25.~~ ~ _B...tR-kar% _ 260__9 .71__ 11 6 __0 -. 0I PorL~oa~__ Bast

(AIXI_1slJ7 i------ an --zZ -9 __c&-2_ n3, ---- --

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A. . _ M.1172 177.~~ Qi

______ s lofs swum __ _m_____ m m-f

IT. 2 V=U & SMIAQ SWGMMW~ REPRT NO.___________WOM M DAME ________

era -~ -- --------

S1N9D TrdtTgEnz CETE OF ORALi INERTIA -

DZCIPIN DATAwd -IM -f -I Su Si __ - - - -o- 3

(LS IT VW. RMOL Ww

443:10tk~q 4 08 q- x--

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VOL No

17.2 -m 5-6e CEAIIO M1U!AL AT REP~ORT 140.

VA MU AI FOW RU AT ____ ______

DESCRIPTIONI DAT!A MORGT TSONTA ETR0GRV SLUG FT4Z10-5

511l _____ ____

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Base ___

41 1.

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X H-

+ + + + : + +

ipqi

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I IO

LT5 APPLICAN* TO O=L 83CIXW SIN 000001.9 AND XXAhUlT

,The following CM's have not been incorporated into "Model Specification,Trainer-Test Group, Guided Missile, (S-133-1006-O-1)".

X.? No, BC? TiTESTG W= WEIW CRARGE

(WS13A-M-)CHAMG fINCO[ORATEDM(W E10" IN 7HIS WRIPTI

"540 Potting & Bonding Deletions for All No*Wadaeben Air Force Base Missiles

606 Revision to CTLI • bailical Bracket- 1 eg-gl. YesSection 49

620 Addition of Static Dissipetors 1 Negl. Yeson 47 Section & Section 49

635 P04 RIF Section Digital Data 3 Negi. YesProgr mer

639 Prevent Interference of Linear . Negi. YesShape Charge with Cable Strap

657 Revision of Ordnance Supports in 2 Ne&L. YesInterstage 2-3

660 Wing III GkC Section & Raceway 3 Negl. Yes_ •_ _Raceway Interface Revisions

Mass properties of other applicable ECP'' have beenincorporated

* D 540 transfors the responsibIlity for sealing the raceway covers fromPlant 77 to Vaombarg. Nowever, the weight Is still considered part ofthe operatiomal mi"sle W is not included in. this report..

UEV SYm ,O

+Wf~PAWT

Ma BCWTl(, /N 0000050

18.1. this sectioni of the document describes the data changes created byconverting a production line Minuteian missile ihato a CTL missile.The mass data reported herein reflect the predicted net changes to beapplied to the total missile mass properties wbea this CTLI secti'onanA the related downstage coponents are installed on a missile. Asupplemental report (see reference 1.1.6) will be issued at VanemnbergAir Force BUe when this CTLI tection Is actually used on a missile.This supplaental report will reflect the actual data gathered ambaais ftring the installation and will thus supersede parts of thisreport. However, past experience has shown that the changes betweenthese two reports will be slight.

The data on the follcwindg pages c .nsist of weight and balance summariescheck lists, and HCP's lists apilicable te this installation. Page 17>sirizes the cuxplete installation mass proptrtiez and consists ofdata Srcm page 176 (average mass properties of downstage components),page 177 (predicted sealant changes), and page 181 (actual weight ofCTLI section BIN 0000050). i, addition, page 178 presents summary checklists by production section as backup data for page 176. Page 182 liststhe engineering change proposals incorporated on the components usedfor this installation.

All data reported in this sectioAn of the document reflect the use ofa linear shaped charge destruct sysbts on the first stage engine perECP 116.

Aerojet weights used in this report reflect the data transmitted toBoeing by Aerojet documeqn 062-olDH-4WOD-I, "Numinal Mass Propertiesand Dispersions for Minuteman CTL'I/Aow" dated January 28, 1963.

Average values have been used for all Boeing items other than theCTLI section which is an actual weight.

4The followtg drawings are incorporated in the above section:

lO-20xJ, httery Instl., Rev H 6-10-63.21-52900, Missile Instl., Rev K 9-19-63.25 -25 4 36, EM 5-6. Instl., DCN J 9-13-63.25-26878, Cable Assy., DCIX J 9-3-63.25-37060, Conduit Assy. DCI B 9-10-63, ADGI S-2O 10-22-63.25-37236, insti. Kxit, DCN C 6-28-63.25-37237, Conduit Supt Set, DCI A 5-10-63.25-37501, 39 Sect. Xnstl., oDC C 11-5-63.29-22321, Timer Instl., DCK D 6-24-63 AWN s-6 9-5-63.

us 4M mo ..V. @10

No W-I 3i3-2' ~~REV SVM-.~.L lfT

TMI, MuZ Kin UIXT RWPORT NO.__________

W-" , n000005 -VATS NRIDUCRunxow DATA MOT SLU GTR0 IWT soFTl~zO-3

________LB) I___ vflooft I_3 if 71 Lt TTw- --&

1 4~ !!n~t - -A__ -

~9 -__ 4~L ~ 2LLt

______ ~Ao z ... _ _ _

8 ± ~~~.3 i. .r________ Ar9

:i. j

Sil.2oo. 1T

28 ase __

4'k5 otrt 1-_ 5& 1

t ~ ~ -- W~u -- -

424&,rtg t 1i-2 25.2 12.2 0

-a -4. - - -, -A a 1. 1.

_ _ Aoro _ -

43_____ Base-

43 + um__ ____ 0

MINS IM - -. M71.26

_ _ ~~ ~ -Je--ts-

DAM* -WL --40 -A -a10 -wIC

- - - -- Ja~ - - - - "o

18.2 VU.M & MLAM MWM CTLX REPORT NO.fAVVA=~ VUW 000 M OATS _____ ______

DESCRUPENDED TATOTAL J~ CENTER OF ORAVIT -NRIA

2..L. _. s7110

Aoro

- 8-. _ _.__, _.___Silo -.

__ _ _ Aero

0 017 - 7- 1 .. .......... . Aslro -,, 71AA. Am•

4 ~roBase_ . _,_r~• _. •-J _i.. ... .z. _ __ ._iT~.'_ o -'

21 Jet 559 10 17. -2 1 . . . ... ..-- -

- • • .~. .Aert...-I_ _Ar_ _-lnAL tr_ . o. tJ.-2... .____ _-__ _ . ._ _ ___• __ _•_-_.•__ , . -

281 i ~Baoe " ,

_ _ - - -2 113.6 123.8_____ ~~Base ____

l -pra- --

u-

A - -AWt) - Silo __ 002__-

SAero

S" , .. ... .. : : e t. . .. . . . .. . . . .. . _ _. . . . ..

- -. -L. - -r

[1A $tax ;7g ; ; _2 15811. 3)2ý

-

r

r

W82U 5-62 M!WNG nODAIJ= AT REPORT NO.VANUMME =X T'OMC BMWZ

DATE _____

CXpENED TOTAL CENTER OF ORAVITY INF.RTIADECRIPTION DATA VW IGIT vfrTO TUSLUG FT4zlO-3

______ ~LB LB~ OG iT v~: 15t TT~

4 .3CTLIH1 94____ _

ALAero ______

S Silo__ --

jAgro -

- ~ ~ . 80 9- - :11~3108 6.Z

I' Base _

IiiSil _,_ _-e

- TOI~4sqmed_ .Aero -

24ertigi 0 -

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.Ea Jkl774tQm I_ er .5 94j 10.__. 1031

(AR2 So 09J~SQ~ft~A Aro _____

Silo - ~ ~ __ 0.

I silo _- U 2_4 Baser

XA -------

2~~00 0 W-lrnc D.3954-534- - .ji i40 D2194-

* aa. -a-a aaa IOUa aaa

C)P

co S

0

64c

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6176

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OTSV

b43

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04xI a S S

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04

64 E4 ~U

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2-5550~-O-11 Ri 0

18. 5 = 53 PROPOSAL ("cp) MIwoPM• oiiAI'PLICABLE9 TO OWL SECTION SIN =00050 AND BTALLATION KIrT

Tbe fullowing ECP's have not been incorporated intc "Model Specification,Trainer-Test Grou•, Guided Missile, (S-133-1006-0-1)".

MTC ~Is. amE TITLE STAGE IWEIGHT WEQIGH CmumG(WS-133A-iBO- 41 CHAE IKC0PP01*ATED

IN THIS RMPRT

540 Pctting & Bonding Deletions for AlNo

IVandenberg Air Force Be Missiles

606 Revision to =TLI Umbilical Bracket- I Negl. YesSecti,)n 49

620 Addition of Static Dissipators Neg. YesOn 47 Section & Section 49

635 PCX R/F Section Digital DataR NeI. .YesPr,:gra _ _r

639 Prevent Interference of rinear 3 Negl. YesShape Charge with Cable Strap

657 Revision of Ordnance Supprts in 2 Negl. YesInterstage 2-3

660 Wing 311 akC Section & Raceway 2 Neg]. YesInterface Rqvisions

Mass properties of other applicable ECP's have beenincorporated

*ECP 540 transfers the responsibility for sealing the raceway covers fruaPlant 77 to Vandenberg. HMwever, the weight is still considered part ofthe operaticaal misaile and is not included in this report.

REV YM A WAW NO. DW-l3943-2

S

19.1 This section of the document describes the date change8 crested byconverting a production line Minuteman missile into a CTL missile.The maw data reported herein reflect the predicted net changew to bea&,plied to the total missile mass prt.perties when this TM sectionand the related dcvmstaepe components are installed on a missile. Asupplemental report (see reference 1.1.6) will be issued at VandenbergAir Force Base when this .J¶ section is actually used on q missile.'this supplemental report will reflect the actual data gathered onbase during the installation and will thus supersede parts of thisreport. Hcwever, past experience has shown that the changes betweenthese two reports will be slight.

The data mn the flluwing pages consists :;f weight and balance summariescheck lists, and LCP's lists ap;,licable tk this installati&n. Page 184sumarizep the cmplete installation mass properties and cunsists ofdata fr,=q page 185 (average mass propertier of d&ownstage components),page 166 (predicted sealAnt changes), and page 1'K (actual weight ofCTLI sectim S/IN 0(30051). In additim. Iage 187 presents summary checklists by production section as backup data for page 185. Page 191 liststhe engineering change proposals inccrpmrated on the c, 4pnents usedfor this installati on.

All data reported in this section 3f the d-cument reflect the use ofa linear shalpd charge destruct systems on the first stage engine perWP 116.

AeroJet weights ised in this repo)rt reflect the data transmitted tcBoeing by Aerojet document 016?-llM-M(PD-j, "Nominai Mass Propertiesand Dispersions for Minutenan CTLI/AOI" dated January 28, 196,3.

Average values have been used for all Boeing Items Ather than the

OTLI section which is an actual weight.

The following drawings are incorporated in the above secti.,n:

l0-20942, Battery Inatl., Rev. H 6-10-63.21-5,900, Missile Irstl., Rev. K 9-19-63.25-254o6, 315 5-62 Instl., Do! J )-13-63.25-26878, Cable Asay., DCN J 9-13-63.2ý-37060, Conduit Assy., DCI• B 9-1,-63, AD=N S-ax) 1o-22-6j.25-37236, Instl. Kit D=I C 6b28-63.25-37237, C,>nduit Supt. Set, DCN A 5-10-63.25-37501, 39 Sect. Instl., DCX C 11-5-63.29-2327, Timer "nUti., DCI D 6-24-63, S-6 9-5-63.

212-63, ANo Si-6 .:9-5.,

"UA QSSZ2400 .. -.V. .'6&2

REV SVM...WL. W*.4 N -13Q03-2,

-Z9.2 WUZ(W & BKLAUC SLO421YF2R 10

£'=L WAPYIBtSIN_00000 a DATE ____

PXPEDID TOTAL CENTER 0F GRAVYMY INERTIA -4 4 DMCRIPTION DATA WSI fIGIT SL* -Tx

-LB - - - -U-14- -

5~ KSilo0

7.l 44. W-vizA-

Aero - - ~--- - -

S Base -- ~--+ - - L iii'-T4. oto~__-Iifi

Z2i1 J Jett 1. V...9&.-AL log-

CAI Q----i- SIgo

'Base. ___

.15- -- -IuSilo- -

_l Aero______ __

j.14VBase

4Z L.r 7aa -5 - - - -2- -

. ~~B-IM3A13-2

19,2 WZZW & 1AANC SUNK= 0= REPORT NO.(AVZMGE VMW CMP rMM) DATE

WEN-DE TOTAL CETER 0 GRA v12 INERTIAS DESCRIPTION DATA ¶~T VIGHT LOGS7VR71LUO FDTTCII

S~AeroMi CTL RYSect~tq___ 2 --..-. -

_ -•Silo

8 • • ______ ...... .I iAero

Z_,2i__& 111A 110• .

2• •_Aero

ilo .... og _- ... ..

Si:- ___-_-___ _ -,

AfL) -Silo___

244. . ... Aero

_-[~~~ ~ ......... 9-o .. .

-.41 Silo 2 -- a

,.~~~ ~ ... ..... .. . .. . ......... _

S.............. A.r•..............-

.___.__-_ _. 8.., • • d_4 - -

Fr = - Dace .... .- ..-- __

4 ~ ~ - - - _ - - - _ - - - _

43 ezf.._ _ _K- - - - - -

19.2 W 5-Q CHU 110MLLD AT REPORT 140.VAUMMIM AIR FORM• BMW

DATC

EPENDD TOTAL INERTIAD&SCRIPTION DATA WIT C OLUG FT4xlO-3ILONG.

J,._ Aero

_ S39Co Sgp z Ae..ro. .. . . .

i Silo ___7f|j|"

•0.! I Portion _ /Base i t/. _

_JAo L I ______ 11 2

I ___ /Base2 I Sil

S... e •orgip ..... . 0___ a--- . ....

~Aero

17 - ...... ....... .•, - .. ...

.1 atem . Aer-q 111 771 71.-

_____~~__ jet___ 7 h 7__21;ett - -.2 53 .6 1.8L1....7

__L__S.l o,• I-9- m-•1• •_ ••.

42 -- 4Aero - 4 ... .T~e

- -aie - - - -

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LV. 4I Bas

031101A sY

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III39 3,2Hi 4 A4 9

19.5 ma k I CHARO PROPOSAL X XMCRPOMTxONAPPLICABLE TO C= S"MOl S/N 0000051 AND DWAILTIN J=

The following BMP's have not been incorporated into 1odel tS1eeification,Trainer-Test GrouT, Guided Missile, (S-133-1006-O-1)".

P sO. =IP TITJLE 9!A WEIM WEI= CHNm(WS-l33A-DO-); cu fINCoaMTM

IN THIIS FaxON

54o Potting & Bonding Deletions for. All No*Vandenberg Air Force Base Missiles i

606 R ision to -C]LX Umbilical Rtacket 1 Negi. Yes"Section 49 I

_�_ __ - 4dlition of Static Dissipators II Wegl. Yeson 47 Section & Section 49

635 P(N •IF Section Digital Data 1e,-,.r. Yes____ ~Programeiir

639 Prevent Interference rf Linear Ie4. YesShape Charge with Cable Strap

657 Revision uf Ordnance Supports in 2 Re4/. YesInterstage 2-3

660 Wing III GIC Section & Raceway J Negl. YesInterface Revisins - . .

)lass properties of other applicable ECP's have beenincorporated

* ECP 5140 transfers the responsibility for sealing the raceway covers from

Plant 77 to Vandenberg. However, the *eight is still considered part ofthe operational missile and is not included in this report.

us 0#6 300 REV. VU

REV SYM..-.L.SC.

AD 406916

END CHANGE PAGES

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