Boilerplate No. 14, House Spacecraft No. 1 Specification, Project Apollo Spacecraft

8/6/2019 Boilerplate No. 14, House Spacecraft No. 1 Specification, Project Apollo Spacecraft

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SID 62-218Fl

BOILER&ATE NO. 14, HOUSE SPAC ECRA FT NO. 1SPECIFICATION

PROJE CT APOLLO SPACECRAFT(Unclassified)NAS 9-150

, 28 Feb ru ary 1962 4272 3

.Approved by


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N O R T H A M E R I C A N A V I A T I O N , I NC . Sf'AC'IC an d INf.'OtMA'I'ION SYS'I'HMS 1)IVISION

CON

CONTENTS

Ti t le P a g ea r a g r a p hSCOPE .

Scope11

1.1.12.2.1

APPLICABLE DOCUMENTS .G e n e r a l . 11

3.3.13.23.2.13.2.1.13.2.1.2

, 3.2.1.33.2.1.43.33.3.13.43.4.13 .2 .23 -4.23.53.5.1

REQUIREMENTS .G e n e r a l .Components .Arrangement .

Command ModuleSe rvi ce Module .Spa cecr aft Adapter .Launch Escape Tow er

P e r f o r m a n c e .Design and Construction .Genera1

G e n e r a l .Equipment .Weight .GeneralGround Support Equipment .

1111333334443444

,.

444

4.4.14.2

QUALITY ASSURANCE PROVISIONSG e n e r a l .Inspection and Tes ts .

444

5.5.15.2

PREPARATION FOR DELIVERY .Airborne Equipment .Transporta t ion .

446.6.1

NOTES .Definitions

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N O R T H A M E R I C A N A V I A T I O N , I N C . SIACI.: an d I NI.C)HMAIION S Y S T I 4 M S 1 ) I V I S I O N

AppendixI-AI-BI-BI- BI- BI-B

APPENDICES

Government -Furn i shed Prop er ty , Cont rac tor -Instal led .

Contractor -Furnished Equipment , Contractor -Instal led, Power Systems .

Contractor -Furn ished Equipment , Contractor -Instal led, Landing Systems .

Cont rac tor -Furn i shed Equipment , Cont rac tor -Instal led, Crew System .

Contractor -Furnished Equipment , Con tractor-Instal led, Communicat ions .Contractor - Furnished Equipmen t , Contractor -

Instal led, Instrumentat ion .

ILLUSTRATIONS

Fi gu re1 B oi l e rp l a t e No. 14 .

Fag e

567

, 89

10

Page2

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N O R T H A M E R I C A N A V I A T IO N . I N C . SI'AA('1S r i r i c l I NI~'0IIMA'L'IONSYS'I'I3MS I ) I V I SI O N/C O N l W i h WW@

1. SGOPE1.1 Scope. - This specif icat ion cov ers the req uire me nts for the House

The boi lerpla te sh al l dem onstra te overa l lpacecra ft Number 1 Boilerpla te .st ru ct ur al and functional compatibility of the Apollo Spa cec raft.2. APPLICABLE DOCUMENTS

2.1 Genera l . - The following documen ts s ha ll fo rm a pa rt of thisspecification:

Government DocumentsAir F o r c eARDCM-80- 1,Volume 1 Designers

Handbook of Instructions f o r Airc ra f t

National Aeronautics and Space Admin istrationNCP200-2 Quali ty Assurance Pr ovi s ion s for

Space Contractors , dated 15December 1961

Non-Government DocumentsSpace and Information Sys tem s Division, NorthAm erica n Aviation, Inc.SID 62-240 Prep arat i on for Del ivery of A irborne

Equipment, Gene ra l Requi rementsF o r

3 . REQUIREMENTS3.1 General . - The configuration of the boi lerpla te sha l l be s i mil ar

to configuration of the prototype Apollo Spacecraft.of the b oiler plat e is shown in figure 1.

The conffguration

3.2 Components. -3.2.1 Arrangement. - The boi lerplate sha l l conta in s t ruo tura l pro-

vis ion s for co mplete s ys tem s installation with the exception of l ive rocketmo tors . The boi lerpla te sha l l include:

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N O R T H A M E R I C A N A V I A T I O N , I N C . SI'AC'IC t i r i c l I NI*Y)IXMKI'lON SYS'I'KMS 1)1 \ 'ISION

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Figure 1. Boilerplate #14-2-

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N O R T H A M E R I C A N A V I A T I O N , I N C . SIACP: urid I NIX)RMAIION SYSIWMS DIVISION

CON(a) Command Module(b) Ser vice Module(c) Spacecraf t Adapter(d) Launch Es ca pe Tower

3.2.1.1 Comm and Module. - The str uc tur e of the com mand module ofthe bo ile rp la te sha l l be a ske le ta l s t ruc tu re and sha l l s imula te the s t ruc tu reof the prototype com mand module.remo vable outer skin . The command module shal l have provis ions formount ing the syst em s in their proper locations .included for mating the co mm and module to the se rvi ce module and thelaunch escap e tower.

The com mand module sha ll include aP r o v i s io n s s h a l l b e

3.2.1.2 Se rv ice Module. - The str uc tu re of the se rv ic e module of theboi lerpla te sh al l be a ske le ta l s t ructu re and shal l s imulate the s t ru ctur e ofthe prototype servic e module . The serv ice module sha l l include a rem ovableouter skin . The servi ce module shal l have provis ions f o r mounting thesys t em s in the i r p roper loca tions .the serv ice module to the spacec raf t adapter and the command module .

Pro vis io ns sha l l be included for mating

3.2.1.3 Spa cec raft Ada pter. - The boilerplate sh all include a prototypeof the spa cec raf t adapter .provis ion s fo r mating to the serv ice module and the S aturn booster .

The spacecra f t adapter prototype s hal l include

3.2.1.4 Launch Es ca pe Tower. - The boi lerpla te sha l l include aprototype of the launch esc ap e tower.sh all include provisio ns f or m ating to the co mmand module.

The launch esc ape tower prototype

3.2.2 Equipment. - The equipment fo r the boi lerpla te shal l includethe equipment l ist ed i n Appendix I-A and I-B.

3 .3 Per fo rmance . -3.3.1 General . - The boilerp late s ha ll be capa ble of acting as a t e s t

pla t f orm for mount ing pr im ary system s to :(a) Evaluate system compat ibil i ty(b) Develop pr i ma ry sy stems t o prototype s ta tu s(c) Evalu ate the interaction of sy ste ms(d) E sta b i sh p r e liminar y oper a t ional pr oc e du re s(e ) Upgrade a l l sys tem s to ful l prototype.

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N O R T H A M E R I C A N A V IA T IO N , I N C . S P A C E and I Nl-~ORMATlON Y S T E M S D I VI SI O N

CONThe boilerpla te sha l l la ter be t rans ferre d to Atlant ic M iss i le Range forfur th er re sea rch and development .

3.4 Design and Constru ction. -3.4.1 General. - The boi lerpla te shal l be constructed of mater i a ls

that will ins ure s tru ctu ral soundness. ARDCM-80- 1, Volume 1 , sh all beused f o r guidance and refe renc e mater ia l i n the design and construct ion ofthe boilerplate.

3.4.2 Weight. - The boilerpla te shal l have a m as s and center ofgrav ity sim ila r to the mas s and center of gravity of the prototype ApolloSpacecra f t .

3.5 Groun d Supp ort Equipment. -. 3.5.1 General , - Ground support equipment shall be req uir ed to

t ran spor t , demo nstra te and tes t the boi lerpla te . The requ irem ents forground support equipment a r e not par t of this specification.4. QUALITY ASSURANCE PROVISIONS

4.1 General . - Quality assu ran ce provisions for the boilerplate shal lbe in a cc ord an ce with the ap plicable port ions of NASA Bu lletin NCP200-2.

4.2 Inspectio n and Te st s. - Inspections and te st s t o de te rmineconformance of the boi lerpla te t'o contract and specification requirementsshal l be conducted pr ior t o delivery to the test si te.5. PREPARATION FOR DELIVERY

5.1 Airb orne Equipment. - Airborne equipment shal l be prep are d forde liv ery i n acco rdan ce with Specification SID 62-240.

5.2 Transportation. - Provis ions s hal l be included to t ransp or t thebo i le rp la te t o the test site.6. NOTES

6.1 Definit ions. - A boilerplate is a s imulated space craf t module forpre-develo pmen tal and /or developmental tes ts leading to the design of aprototype module.

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N O R T H A M E R I C A N A V I A T I O N , I N C . SPAACt.2 and I NI'ORMATION SYSTEMS DIVISION

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Appendix I - AGovernment-Furn ished Pr ope r ty , Cont racto r - Ins ta l l ed

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Armendix I -B

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Cont rac to r-Furnished Equipment , Co ntracto r-Ins ta l led

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N O R T H A M E R I C A N A V I A T I O N , I N C . SI'AC'I.: tirid 1 N I ~ ~ O l ~ M A ' ~ I 0 NYS'l 'HMS r)IVISION

Appendix I-BContractor- Furnished Equipment, Contractor-Ins ta l led

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Appendix I - BContractor- Furnished Equipment, Contractor-Ins ta l led

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N O R T H A M E R I C A N A V I A T I O N , I N C . SI'AC'H n r i r l I N I * ~ O I ~ M A T I O NYS'I'I.:hlS 111V I S I O N

Appendix I - BCon tractor-F urnish ed Equipment, Contractor-Ins ta l led

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/ ,-N O R T H A M E R I C A N A V IA T IO N , I N C . S1'AC.E and I NFORMXI'ION S\ STEMS DIVISTO.\

Appendix I-BContractor-Fu rnished EquiDrnent, Co ntractor-Installed

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