Project Apollo End Item Specification Boilerplate Number 26

8/6/2019 Project Apollo End Item Specification Boilerplate Number 26

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Accession No. ?&61-64-Copy .No. 657' S I D 63-695

PROJECT APOLLOEND I TE M S P E C I F I C A T I O NBOILERPLATE NUMBER 26 (U )

5 March 1964 NAS9-150

Paragraph 4.2, Exhibit I.

This document contains iUnited States within theSection 793 and 794. Itsmanner to an unauthorized

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TABLE O F CONTENTSPa rag raph

1.1.11.1 .11 .1 .21 .1 .322 .12 .1 .12.1 .22.23.3. 13. 1.13 .1 .23. 1.2. 13. 1.33. 1. 3.13. 1. 3. 23. 1. 3. 33. 1.43. 1. 4. 13. 1.53. 1.63 .1 .73. 1.83. 1.93. 1.103. 2

3.2. 13.2. 1. 13.2. 1. 23.2. 1. 3

SCOPEScopeSpecification OrganizationMis sionObj ectiv es

APP LIC ABL E DOCUMENTSApplicabilityGovernment DocumentsNon-Government DocumentsP r e c e d e n c e

REQUIREMENTSGenera lWeightMat erial sFabr ica t ionDesign Cri ter iaElectromagnet ic Inte rf e renc eEnvironmentCheckout Prov ision sInterchangeabilityInterchangeability of Electronic EquipmentReplaceabilityFinishIdentif ication and MarkingIdentif ication and T race abil i tyLubricat ionReliability

CONFIGURATION

LAUNCH ESCAPE SYSTEM (LES)Nose ConePitch Control Motor CoverTower Je t t i son M otor

P a g e

444444444455555556

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P a r a g r a p h3.2. 1 .43.2.1.53.2.1.63.2. 1.73.2. 1 .83.2. 1.8.13.2.1.8.23.2. 1.8.33.2. 1.8.43.2. 1.8.53.2. 1.93. 2. 1. 103. 2. 1. 11

TABLE O F CONTENTS (CON'T)Launch Esca pe MotorS t ruc t u ra l Sk i r tLaunch Escape TowerLES Tower Separat ion SequencerE l ec t r i ca l Sys temMission SequencerL E S E l ec t r i ca l Wi ri ng H arnes sHotwir e Ini t ia torsHotwire Fi r ing UnitsPyro technic Bat t e r i esUmbi l ical Sys emPyrotechnic Sys emLES Tower Separ at ion Sys tem

3.2 .2 COMMAND MODULE3.2.2.1 Command Module St ru ct ur e3.2.2.1.1 Cabin Housing3.2.2.1.23.2.2 . 1 .3 Forw ard Crew Compartment3. 2.2.1.4 Aft Cre w Com part men t3.2.2 .1 .5 Apex For war d Compartment Heat

Shield Cover3. 2. 2. 1. 5.1 CM Insu latio n3.2.2.1.6 Ac ces s Hatch3.2.2.1.6.1 Acc ess Doors3.2.2.1.7 Sc imi tar Antenna3.2. 2. 1.8 Dummy CM Vent3.2.2.1.9 Miss on Sequen cer3.2.2.1.10 Ele ctr ica l Power Sy ste m (EPS)3.2.2.1.11 Rand D Communicat ions Equipment3.2.2.1.12 Rand D Inst rume ntat ion Equipment3. 2. 2. 1.133.2.2. 1.14 CM-SM Attach Sy st em3. 2. 2.1.15 CM-SM Se pa ra ti on

Forwar d Bulkhead and E gr es s Tube

Environmental Control System

P a g e77777788888889991 0

1 0101010101111111111111112121212123.2.3 SERV ICE MODULE3.2.3.1

3.2.3.23.2.3.33,2,3,4

SM React ion Control Syste m (RCS)CM-SM Fa irin g 12SM Inse r t 12Adapter 1 2

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TABLE O F CONTENTS (CON'T)

P a r a g r a p h3 . 2 . 3 . 5 SM Purg ing3. 2 . 3 . 6 SM Prot ect iv e Bulkhead3 . 2 . 4 LAUNCH VEHICLE3 . 3 PERFORMANCE3 . 3 . 1 T r a je c t or y P a r a m e t e r s3 . 3 . 2 Fl igh t P la n4. QUALITY ASSURANCE4 . 1 General Qual ity Assu ranc e Provis i ons4 . 2 Principal Contractor I s Quality4 . 2 . 1 Reliability Data4 . 3 Examination4 . 3 . 1 Components4 . 4 T e s t s

A s s u ra n c e P r o g r a m

5. PREPARATION FOR DELIVERY5.1 Pre ser vat ion , Packaging, and Packing

6. NOTES6 . 1 Delivery of Mo dules

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P a g e121213131313131313131314141414

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LIST O F ILLUSTRATIONSP a g e

15Boilerplate Number 26 ConfigurationAPPENDICES

A-1A-2B-1B - 2B-3B -4B -5B -6B -7B -8B-9B-10B-11B-12B-13B-14B-15B-16B-17B-18B-19B -20B-21B -2.2B -23c-1c 2c 3c 4c - 5C -6c 7C-8c 9

AABBBBBBBBBBBBBBBBBBBBBBBCCCCCCCCC

DrawingsDrawings (Continued)Pr oc es s Specif ica tionsPr oc es s Specifications (Continued)P ro ce ss Specifications (Continued)Pr oc es s Specifications (Continued)Pr oc es s Specifications (Continued)Pr oc es s Specifications (Continued)Process Specifications (Continued)Pr oc es s Specifications (Continued)Pr oc es s Specifications (Continued)Process Specifications (Continued)P ro ce ss Specifications (Continued)Process Specifications (Continued)Process Specifications (Continued)P ro ce ss Specifications (Continued)P ro ce ss Specifications (Continued)Pr oc es s Specifications (Continued)P ro ce ss Specifications (Continued)Process Specifications (Continued)Process Specifications (Continued)Process Specifications (Continued)Process Specifications (Continued)P ro ce ss Specifications (Continued)Process Specifications (Continued)Mate rial SpecificationsMaterial Specifications (Continued)Material Specifications (Continued)Material Specifications (Continued)Ma terial Specifications ( Continued)Material Specifications (Continued)Material Specifications (Continued)Material Specifications (Continued)Material Specifications (Continued)

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APPENDICES (CON'T)

CCCCCDDE

Mater ial Spec ifica tions (Continued)Mat eri al Specificati ons (Continued)Material Specifications (Continued)Mater ial Spec ifica tions (Continued)Mater ial Spec ifica tions (Continued)Procurement Specif icationsProcurement Spec ifica tions (Continued)Flight Instrumentation

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P a g ec - 1 0c - 1 1c - 1 2C-13C-14D-1D-2E-1

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PROJECT APOLLOEND ITEM SPECIFICATIONBOILER PLATE NUMBER 26

1. SCOPE1. 1 Scope. -Apollo spa cec raft consist ing of a launch escape syste m (LES), commandmodule (CM) , se rv ic e module (SM), and adap te r he re inaf te r re fe r re d toas Boi lerpla te Number 26.

This specif ica t ion def ines the requirements fo r a s imulated

1.1. 1follow s:Specification Organization. - This specification i s organized a s

Basic sectionAppendix A - DrawingsAppendix B - Process Specif ica t ionsAppendix C - Material SpecificationsAppendix D - Procu reme nt Specif ica t ionsAppendix E - Flight Instrumentation

1.1.2mi cr o -meteoroid experiment .

Mission. - Boilerplate Number 26 i s the second vehicle fo r the1.1. 3 Objectives. -vehicle qualif ication and micrometeoroid experiment.will be determ ined by MSFC.

Boilerplate Number 26 shal l be used fo r the launchTes t ob jec t ives

2. A P P L I C A a L E DOZUMEiuTS2.1the date of contr act for m a par t of this specification to the extent sp ecifiedherein .

Applicability. - The following documents of the is su e in e ffect on

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2.1.1 Government Documents. -SPECIFICATIONS

MIL-E-5400 Electronic EQZlipment, A ircr af t,General Specification for

MIL-I-85 0 Interchangeability and Rep laceabilityof Component Parts for A ircraft andM issiles, Specification fo r

M L L - L - ~ ~ ~ O Lubricating, Aircraft, GeneralSpecification or

MIL-R-27542 Reliability Prog ram Requirementsfor Systems, Subsystems, andEquipment, Specification fo r

STANDARDSMIL-STD- 130 Identificatfon Marking of U.S.

Military Prope rty

2.1.2 Non-Government Documents.SPECIFICATIONS

North American Aviation, Inc. ,Space and Inform ation Systems Division (NAA/S&ID)MA 0116-012 Prep aration for Delivery and Transport

of Apollo Boilerplates, Specificationfo rMC 999-0002B Electromagn etic Interfe rence Controlfor the Apollo Space System,

Specification fo r

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W. ,. ' .*

OTHER DOCUMENTSSID 62-109 Genera l Tes t Plan, Research andDevelopment for P ro je ct Apollo

Spacecraft , dated Ma rch 1963SID 62-223 Apollo P ro gr am PlanSID 63-143 Actual Weight and Balance

Report Boilerplate Number 26SID 63-313 Apollo M as te r Spac ecra ft

Sp e c i ica tionDRAWINGS

North Ame rican Aviation. Inc.Space and Information Systems Division (NAA/S&IDB14-000024 Fin ish Specificatio n Apollo

Boilerplate, Complete~1 4 - 0 0 0 0 0 2 - 2 5 i G e n e ra i A s se m b iy , B o il e rp la t e

Number 26B15-000002-221 Ge ner al Ass emb ly, LES 15Bl6-000002-281 Gen eral Ass emb ly, CM 26B17-000002-221 Ge ne ral Ass emb ly, SM 11B18-000002-251 Ge ne ral Ass emb ly, Adapter 16B18-320113 Str uct ure , In se rt

2 .2as follows:

Precedence . - T h e o r d e r of precedence in ca se of conflict will be(a ) The contract(b) This specification( c ) Other documents r efere nced herein

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3. REQUIREMENTS3. 1 Gen era l. - The fol lowing parag raphs del ineate the req ui re men tsfor des ign , fabr ica t ion , assem bly , and per formance fo r Boi l e rp la teNumber 26. Systems and subsystems development plan philosophy isreflected i n SID 62-223, Apollo Pr o g ra m Plan.3. 1. 1 Weight. - Weight, ce nte r of gravity , and mom ents of ine rt i adata fo r Boi lerplate Num ber 26 shal l be presen ted in Specif icationSID 63-143.3. 1. 2and load cr i ter ia .

Materia ls . - Ma teria ls shal l be compat ible wi th design, weight,3. 1. 2. 126 emphasize employment of prove n manufacturing techniques and methodsto the gre ates t possible extent."off - he - shelf ' components fab rica ted by dependable ma nu fa ctu re rs .

Fabricat ion. - Str uc tur al design concepts of B oilerplate Numbe rMaximum use shal l be m ade of developed

3. 1 . 3rat ional design principles a s specifie d i n Spec ification SID 63-313.

Design Cr i ter ia . - Design c r i t e r i a sha l l be in accordance wi th3. 1. 3. 1con trol sha ll be i n ac co rd an ce with Specification SID MC 999-0002.

Elect romagnet ic Interference. - Elec tromagneti c in t e r fe ren ce3. 1. 3. 2plate Number 2 6 sha l l be a s specified in Specificat ion SID 63-313.Environment. - The envi ;onmental design cr i te r i a for Boi ler-3. 1. 3. 3designed with provisions f or sys tem and integrated sy ste m checkoutand test capabi l i t ies .

Checkout Provisions. - Boi lerplate Number 26 shal l be

3. 1. 4Pr og ra m shal l be in accor dan ce with Speci f icat ion MIL-1-8500 and s hal lapply to all completely f inished as sem bl i es , components , and pa rtswhich sh al l be capable of being readily inst al led , remov ed, o r replac edwi thout a lternat ion, misal ign ment , o r damage to pa rt s being instal led orto adjoining parts . No fabricat ion operat io ns, such a s cut t ing, f il ing,dr i l l ing , reaming, h amm ering , bending , p ry ing , o r fo rc ing , sha l l berequi red for instal la t ion.

Interchangeabil i ty. - Interchangeabil i ty a s defined fo r the Apollo

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3 . 1. 4. 1of elect ronic equipment shall be in acco rda nce with Specification MIL-E-5400,wh ere applicable .Pr og ra m sha l l r equ i r e that mechan ical and e lec t r i ca l in te rchangeab il i tysha l l ex i s t between l ike assem bl ies , subassembl ies, and replaceable pa r tsbe eas i l y effected without physical or e le ct r ica l modif icat ion to any pa r t ofthe equipment, including ; cabling , wir ing , and mounting and withoutresor t ing to se lec t ion ; however , ad jus tment , t r imming , o r ca l ib ra t ion maybe made .

Inter chan geab ility of Ele ctr on ic Equipment. - Interchangeabil i tyInterchangeab il i ty of elect ronic equipment for the Apollo

3. 1. 5P ro g ra m , shall be in acc ord anc e with Specification MIL-1-8500 andshal l apply to pa r ts which may requ ire addi tional work o r operat io nsduring installat ion. This may include such additional operation s a sdri l l ing, reaming, cut ting, f il ing, t r imm ing, shimming, or o ther mea ns ,norm al ly a ssoc ia ted with ins ta l l ing the or igina l assembl y in to the end i tem.Replaceable pa r ts shal l be des igned to per mi t rep lacement under f ie ldmain tenan ce conditions.

Replaceability. - Replaceability, a s defined for the Apollo

3 . 1. 6 Finish . - Finish requirements shal l be a s specif ied in SID DrawingB14-000024.3. 1. 7in acc ord anc e with Specification MIL-STD-1 SO.

Identification and Marking. - Identif ication and markin g shall be3 . 1. 8sha ll be in acco rda nce with the req uir em ent s of Specification SIDMA 0201 -0208.

Identif ication and Tracea bil i ty. - Identif ication and trace abil i t y

3 . 1. 9 Lubrication. - Lubricat ion of com ponents , where requ ired, shal l bein acc ord anc e with the requ irem ents of Specification MIL-L-6880.petro leum -base lu br icants sh al l be used.base, f luorolube, oxylube 702, and dry film type. Lubr icatio n shal l notcaus e any tox ic o r f l ammable subs tances to occur in the CM o r i n th eerrvi onlr-erztal cnnt1-01 ys tem.

NoLubr icant s sh all be of the si l icone

3 . 1. 10 Reli abili ty. - An integrated re l iabi l i ty pro gra m, general ly inacc ord anc e with Specification MIL-R-27542 , sha ll be conducted throughoutthe design, development, and fabrication, and checkout and acceptance ofBoi lerpla te Number 2 6 .

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3. 2 Configuration, -i n F i gu re 1.B14-000002-25 1.

The configurat ion of Boilerp late Num ber 26 i s shownFor detai led configurat ion information, re fe r to SID Drawing

3.2. 1 Launch Escape System. - The LES sha l l cons ist of the followingma jor components:

(a ) Nose cone(b) P i t ch cont ro l motor cover(c ) Tower j e t t ison motor(d) Launch escape motor (empty cas e)( e ) S t ruc t u ra l sk i r t( f ) LES tower(g) LES tower separa t ion sequencer

3 .2 .1 . 1 Nose Cone. - The LES nose cone sh al l provide cap abil i t ies fo rmounting, in the nose cone apex, a NASA furnishe d Q-Ball as se mb ly andwiring fro m the Q-Bal l in terfac e to the booster interface .fo r accomodating 1,50 0 pounds of lea d ba l la st within the bal la st enc losu resha l l a l so be made .

Provi s ions

3. 2. 1. 2 Pitch Control Motor Cover. -the pi tch co ntrol mot or nozzle opening. A cover shal l be provided to close3. 2. 1. 3 Tower Jet t i son Motor. - The tower je t t i son motor shal l be asol id propel lant moto r 55. 6 inches in length and 26 i nches i n d i am e te r .The motor shal l have two fixed thr us t nozzles canted 30 degre es fr om themean m otor cen te rl ine . The resul tant thru st axis shal l be located 2. 5degree s p lus o r minus 30 minutes f ro m the mean m otor cen te r l ine ofthe pitch plane.which includes the inter stag e s tr uc tu re , sh al l develop 33,000 pounds of thr us tand sha l l f i re fo r 1. 2 seconds.pyrogen type ign iter which sh al l ut i l ize two hotwire ini t ia tors .

The je t t i son moto r shal l weigh approximately 534 pounds,The rock et moto r shal l be igni ted by a

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SPACE and INPORhlATlON SYSLEhlS I ) I \ . I S I O NN O R T H A M E R I C A N A V I A T I O N , I N C .co-3.2.1.4 Launch Esc ape Motor .iner t empty l aunch escape mo to r case with nozz les removed .183 inches in length and 26 inches in diame ter and shal l provide inters tagest ru ctur e between the LES j e t t ison motor and s t r uctu ral ski r t .

- The launch escap e motor shal l be anIt shal l be3.2.1 .5 St ructur al Ski r t . - A s t ruc tura l sk i r t ass embly shal l be u t i l izedto mount the launch esc ape motor to the tower.of a forged r ing with longer ons, welded to a sh ear skin, that shal l t ra ns feruni form load fr om the launch escape motor to four points a t the launch escap etower legs.

The ski rt shal l be construc ted

The st ru ctu ra l s kir t shal l be bolted to the LES tower.3 .2 .1 .6 Launch Esc ape Tower. - The launch esc ap e tower shal l be afour- legged welded tubular a l loy, t runcated recta ngular cross -sect ione dpy ram id, 120 inches in length with a bas e 46 inches by 50 inches. Thetower shall fo r m the intermed iate str uc tur e between the CM and the launchescape m o t o r . At the bottom of the tower, quick-r elease mec han ism sshall be incorp orated to at tach the tower to the CM inner s t ructure .tower s t ru ctur e shal l be cove red with ablative ma ter ia l , Buna-N rubbersixty per cent s i l ic a fi lled.

The

3.2.1.7 LES Tower Sep arat ion Sequencer ,sequen cers sha l l con t rol , upon receipt of tower separat ion signal , (1)launch escape tower separat ion and (2) ignition of the LES jet t ison mo tor ,The separat ion s ignals shal l be t ransmi t ted through redundant bus ses ,A and B,

- The two LES tower sep ara t ion

3-2 .1 .8 E lec t r i ca l Sys tem. - The LES elect r ical system shal l consis tof th e following m aj or components:(a) Mission se quencer ( located in CM)(b) Wiring ha rn e s se s and associated at tachm ents(c) Hotwire ini t ia tors(d) Hc?twire fi ri ng units(e) Assoc iated pyrotechnic bat te r ies , wir ing, and at tachments .

3 .2.1 .8 .1 Missio n Sequencer . - The mission sequencer shal l automat ical lycontro l LES tower separ at ion s equen cer and CM-SM separat ion. Otherfunctions of the miss ion sequencer a r e unde termined a t t h is da te.

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3 . 2. 1. 8. 2sh all be bonded t o t he ex t e r io r of the l aunch escape motor and asso c ia t e dredundant har ness es sha l l be in t egra l t o the tower s t ruc ture . The wi r ingha rn es se s shal l provide the mea ns of connecting the roc ket moto r andsepara t ion c i rcu i t s with the sequence con t ro l l e rs and the ins t rumenta t ioncomponents with the comm unicat ion s equipment.shal l have a breakaway type plug that shal l pe rm i t the ha rn es s to be detached,at the separat io n plane, when the launch escap e tower i s je t t i soned.

LES Elec t r ica l Wiring Harne ss . - Redundant wir ing harnesses

E ach tow er s t ruc t u re ha rne s s

3 . 2. 1. 8. 3 Hotwire Ini t iators. -high re s i s t an t wi r es th readed in to pyro technic ca r t r idg es which f i re theigni t er of the rocket motor . The ini t ia t ors shal l be redundant fo r inc rea sedrel iabi l i ty.

The hotwire ini t ia t ors contain two el ect r i cal

3 . 2. 1. 8. 4 Hotwire Firing Units. - The hotwire f i r ing uni t s sha l l bepyrotechnic cart r id ge s which s hal l be detonated by cu rre nt passing throughthe h igh res i s t an t e l ec t r i ca l ho twire in i t ia to rs . The pyro technic car t r idge sshal l then f i re the rocket moto r igni ter s .3 . 2. 1. 8. 5 Pyro technic Bat t e r i es . - The pyro technic ba t t e r i es fo r the LESshal l be housed in the CM. Ele ct r ica l wir ing sh al l provide the mea ns bywhich cur ren t wi ll be c ar r i ed f ro m the ba t t e r i e s to the pyro technic f i r ingunits.3 . 2. 1. 9 Umbilical System. - The umbi l i ca l sys t em sha l l con ta in e l ec t r i c a lwiring between the CM and LES. The umbil ical sha l l be detached by str ai non the lanyard type disconnect when the LES jet t i so n mo tor cau ses CM-LESsepara t ion .3 . 2. 1. 10the following:

Pyrotechnic System. - The pyro technic sy s t em sha l l cons i s t of( a ) Pyro technic ba t t e r i e s(b) Hotwire ini t ia tors(c ) Disconnect asse mbl i es .

3.2. 1. 11 The LES t ower separa t ionsy ste m shal l con sis t of explosive bol t s , us ed for LES tower- CMat tachme nt , and flexible l in ear shaped explosive cha rg es placed beneaththe four a t tachment explosive bol theads that s ec cr e the tower to the CM.

LES Tower Separa t ion System. -

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Redundant hotwire in i t iato rs shal l be us ed to detonate the explosive boltsand f lexible l in ea r shaped explosive charge s. The hotwire ini t ia tors shal lbe actuate d by 28 volt dc s ignals which s hal l be rece ived fr o m the redun dantL E S tower sepa rat ion sequencer . To accom pl ish LES tower je t t ison, thetower separa t ion se quenc er wi l l s imultaneously:apply detonation signals t othe explosive bol t in i t ia tors and the tower je t t i son mot or f i r ing uni t s . TheLES ass emb ly wil l be re l eased and prope l led c l e ar of the boilerplatet r a j ec t o ry .3. 2. 2 Command Module. - The CM shall consist of the following:

( a ) CM s t ruc ture(b ) Miss ion sequencer( c ) Elec t r i ca l power sys t em(d) The R and D communicat ions equipment(e ) The R and D inst rumentat ion equipment(f ) Environmental Control System (ECS).

3.2. 2. 1141 inches high and 154 inches in d iam eter a t the b ase wi th a net weight of

Command Module Structure . - The CM shal l be of conical design,approximate ly 9000 pounds.with a skin thickne ss of appr oxima tely 0. 190 inch.provided a t the fo rwa rd bulkhead to engage the launch escape tow er legs. Thecon figu ratio n of th e CM sha ll be in ac co rd an ce with SID Drawing B16-000002-281and shal l be s im ila r to the ul t imate s pac ecr aft CM. All equipment in the CMshal l be placed a s ne ar a s possible to the posit ion to b e occupied in theult im ate sp ace cra ft CM. The CM st ru ct ur e shal l include the fol lowing:

The s t ruc ture sha l l be fabr i cated f r om a luminumAttach fit t ings shal l be

(a ) Cabin housing(b) Heat sh ie ld s t ruc ture(c ) Sepa rat i on sys t em

3. 2. 2. 1. 1al loy welded into two s ubass embl ies , (1) the forw ard crew com partme ntand (2) the a f t c rew compar tment .together and the af t sk i r t f r am es and sk in sha l l be a t t ached by mechanica lfa s te n e r s.

Cabin Housing. - The CM shel l sha l l be co nstr ucte d of aluminumThe subass embl i es sha l l be bo l ted

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3.2.2. 1 . 2 Fo rw ard Bulkhead and Eg re ss Tube- -s t ru c ture sha l l cons i s t of a double skin with r iveted s t i f feners .sk in sha l l be a t t ached to s t i f fe ners by b l ind fa s t en ers .con sfst of a welded sh eet tube of aluminu m welded to the f orw ard bulkhead.A cov er plate shal l be bol ted to the top of the e gr es s tube.

The for war d bulkheadThe closeoutT he eg re s s t ube sha l l

3 .2 .2 . 1 .3shal l consis t of mul t i -s t i f fene rs welded to the oute r skin. The s t i f fe ner sshal l consis t of four main lon gerons at tache d to the launch esc ape towerf i tt i ngs in the forw ard bulkhead and t e rmin a te in the mid-r ing sp l i ce jo intat the aft end of the for wa rd sect io n of the c re w compa rtme nt .secondary longerons sha l l be u t i l ized for load t rans fer f rom the forwardbulkhead to the mid -rin g. The remain ing s t i f fen ers sha l l as s i s t t he sk ini n r e s i s t ing a i r l oads .

For war d Crew Compar tment . - T he fo rw ard c rew com part m en t

Seve ra l

3. 2. 2. 1. 4sha l l con sist of a sidewall with st i ffe ner s, cor resp ond ing to those of th eA f t Crew Compartment . - The aft sect ion of th e cr ew com partmen tforward sec tion of the c re w com par tmen t , f rom the mat ing aft sect ionof the cre w compa rtment mid-r ing to the machined r ing forging at thejunction of the sidewall and the floor.3. 2. 2. 1. 4. 1 Aft Hea t Shield. -a s nec essa ry , sha l l be added to the aft hea t sh ie ld to provide acc es s to themicro-m eteoroid pyrotechnic t ie point . A 15 inch hole shal l a l so be addedto the aft bulkhead. A doubler , door, and sea l shal l be included.

A 15 inch diamete r hole , wi th reinfo rcemen t

3 .2 .2 . 1 .5 Apex Forw ar d Com partment Heat Shield Cover. - The apexforward compar tment hea t sh ie ld cover s t r uc tur e sha l l fo r m the forwardsect ion of the CM st r uc tur e and shal l con sis t of an aluminum al loy skinand s t i f feners ut i l iz ing r ive ted and bol ted const ruct ion.sk in sha l l be used to ins ur e a smooth sur face .aluminum.

A l ightweight in ne rThe nose cone wi ll be

3. 2. 2. 1. 5. 1 The CM exte r io r s hal l be provided wi thsui table cork insulation to pro tect the module f ro m aerodyn amic heat ingCM Insulation . -

during the launch phase.3 .2 .2 . 1 .6in te r io r .and sha l l be bolted into place.the head of the c en te r couch posi t ion.

Acc ess Hatch. - The main ha tch sha l l p rov ide acc es s to the CMIt shal l be located in the CM sidewal l ove rThe hatch sha l l be co nst ructed of re in forc ed aluminum plate

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c I' * *"9

3.2. 2. 1.6, 1 Access Doors . - Access do ors shal l be provided in the s ki r ts t r uc tur e for servicing the heat shield at tach s t ruts .be provided in the forward c rew compar tment s t ruc tu re , 9 0 deg rees apa r t ,fo r t e l eme t ry an tennas .

Fo ur openings shal l

3. 2. 2. 1. 7located on the lowe r sk irt of the CM at s ta t ion Xc 24. 12.be ci rcumferent ia l ly centered 22 . 32 i nches f rom the - Z xis toward the-Y xis. The o ther sha l l be cen te red 3 .91 inches f ro m the t Z axi stoward the t Y axis .and aerodynamic chara c te r i s t i cs of the u l t imate spacecraf t sc im i ta rantenna6.

Scimitar Antenna. - Two sim ulated sc imi tar antennas shal l beOne antenna shall

The antenna shal l simulate the si ze , wkight , shape

3. 2. 2. 1. 8vent sha l l be ins tal led on the CM.and gl as s lam inate with an at taching holddown sec ure d to the SM.

Dummy CM Vent. - A dummy CM aft equipment compartmentIt shal l be con stru cted of sheet me ta l

3. 2. 2. 1. 9con trol LES-CM and CM-SM separat ion.Mission Sequencer . - The mission sequencer shal l automat ical lyOth er possib le functions of themi ss io n sequ enc er wil l be at the disc ret ion of the MSFC.3 . 2 . 2. 1.10and distr ibute ele ctr ica l power and shal l con sist of the fol lowing ma jo r

Elec t r i ca l P ower Sys tem (EPS). - The CM EPS shal l supplycomponents:

(a) Main power b at ter ies(b ) Py ro -ba t t e r i es( c ) Elect r ical dis t r ibut ion system

(1 CM-LES umbil ical(2 ) CM-SM umbilical.

3 . 2. 2. 1. 11r equ i r em en t fo r R and D communicat ions equipment in BoilerplateNumber 26.

R and D Communications Equipment. - NAA/S&ID ha s no3.2. 2. 1. 12requ i r em en t fo r R and D instrume ntat ion equipment in BoilerplateNumber 26.

R and D Instrumentat ion Equipment, - NAA/S&ID ha s no

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3 . 2 . 2. 1. 13for an ECS in B oi lerplate Number 26.Environmental Control System. - NAA/S&ID ha s no req ui re men t

3. 2. 2. 1. 14pos i tive t ension t i es th rough the th r ee SM comp ress ion pada .pre loaded t ens ion s t ra ps sha l l be sec ured to the CM inner s t r uc tur e and theSM at the upper beam ,

CM-SM Attach System. - The CM-SM at t ach s ys t em sha l l u t il i zeT he t h r ee3. 2. 2. 1. 15not provided for Boi lerplate Number 26 .CM-SM Separation. - Capaljil5ty for CM-SM sepa ra t i on i s3. 2. 3and 154 inches in d i am eter ,const ruct ion consis t ing of skin, longeron s, and fr am es .

Ser vice Module. - The SM shal l be a cyl inder 124 inches in lengthThe s t ruc ture sha l l be a luminum semi -monocoque

3 . 2. 3 . 1be instal led at station 325.SM Reaction Control System (RCS). - The SM RCS engines shallThe RCS quad packages sha l l be dummy mot or ss imula t ing the s i ze , weight, shape , l oca tion, and aerodynamic char ac te r i s t i csof the ul t imate s pac ecr aft RCS.3 . 2. 3 . 2 CM-SM Fair ing, - The boi lerplate shal l include a fai r i ng betweenthe CM and SM.lef t , by the curva ture of the CM aft heat shield , when the CM i s mate d tothe SM and i s res t ing on the comp ress ion pads ,mechani sm and a fixed CM-SM u mbi l ical sh al l be ho used within thefa i r ing .ab la t ive mater i a l .

This fa i r ing sha l l provide c los ur e of the gap which wi l l beAn iner t se para t ion

The fai r ing shal l be removable and sh al l be sur face d wi th co rk

3.2. 3. 3and SM.const ruct ion 52 i nches in l ength and 154 inches d iameter .

SM Insert. -The ins ert shal l be a n aluminum cyl inder of semi-monocoqueThe SM ins ert shal l be located between the ada pter3. 2. 3 . 4monocoque const ruc t ion 9 2 inches i n length a d 154 inches d iamete r .It shal l be located between the SM i nse r t and the S-IV stage of theS-I Launch Vehicle.

Adapter. - The adapter sha l l be a n a luminum cyl inder of s em i -

3. 2. 3. 5 SM Purging. -GSE GN2 purging lines. Provi s io ns sha l l be made in the SM to a t t ach3 . 2. 3. 6 SM Protect ive Bulkhead. - A pro tect iv e bulkhead shal l be at tachedto the lower r ing in the SM ada pter . This bulkhead shal l be an a i r conditioningba r r i e r t o i so la t e t he S-IV cool ing sy s t em f ro m the adap ter cav ity .

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3. 2. 4wil l be Saturn I Block I1 configuration.Launch Vehicle. - The launch vehicle for Boilerplate Number 263. 3be outlined by th e MSFC.

Per formance . - The performa nce of B oilerp late Number 26 will3. 3. 1 T r a j e c te c t o r y P a r a m e t e r s . - To be d ete rm ine d by the MSFC.3 . 3 . 2 Flight Plan. - To be d eterm ined by the MSFC.4. QUALITY ASSURANCE4. 1 General Qual ity Assu rance Provis ions . - The principal contract or(S&ID) shal l be responsible for the p erfor manc e of all inspectionrequ i rements a s specif ied herei n . Except a s o therwise specified , thepr inc ipal contra ctor ma y ut i l ize his own or any other inspect ion faci l i t iesand ser vi ce s acce ptabl e to the NASA. Inspection re co rd s of the examina-tions and test s shall be kept complete and availab le to the NASA a s specifiedin the con t rac t.4. 2 Pr inc ipa l Cont rac to r ' s Qua li ty Assurance Prog ram. - The pr incipalcon t rac to r sha l l e s tab l i sh a qua li ty ass ura nce p ro gra m in accordance withthe requ i rements of paragraph 2. 5 of Exhibit A of the contr act . Inspectionsand tes t s to determ ine conformance of Boi lerpla te Number 26 to con t rac tand specif ica t ion require ment s shal l be conducted pr io r to sl;bmission of thear ti cl e to the NASA fo r acceptance.4. 2. 1his tor ian and accumulate appl icable data on spacec raf t tes ts , p lans , and

Reliabil i ty Data. - The pr incipal contr actor shal l ac t a s a t e s tp e r f o r m a n c e from prep arat io n to del ivery .qual i ta tive and quant i tive ass ess me nts of re l iabi l i ty and perfo rman ce ofeach syst em , an d of the ult im ate spac ecraf t .o the r appropr ia te da ta , such a s acceptance data , shal l be in tegrated withtha t accumula ted f ro m pr io r t e s t s to f o rm a s s e s s m e n t s . Thus, aprobabil i ty of su cc es s ma y be provided fo r any given phase of the miss ion.

The data shal l be used inThis data , together wi th

4. 3for acceptance shal l be subjected to a visua l examinat ion to dete rmin econformance io ma te r ia ls , des ign, construct ion, d imensions , color andf inish , product mark ing, and workmanship .

Examination. - Each assembly and a l l ma jo r components submit ted

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4. 3 . 1 The pr incipal contractor shal l as ce r ta in that ,p r io r to assembly, all par t s , components , a ssembl ies , and sys temsprocured under separ ate specif ica tions o r drawings hs-. been inspected,tes ted, and accepted in accordance with their respect ive specif ica t ionso r d rawings ,

Components. -

4. 4 Tests . - Each assem bly, m ajor component, an d sys tem submit tedfor acceptance shal l be subject to performance tes ts as specified inapplicable documents including Specification SID 62 - 109.5. PREPA RATION FOR DELIVERY5. 1 Pre ser vat ion , Packaging, and Packing. - Preservat ion, packaging,and packing shall be in accordanc e with the principal co nt rac to r 'sproce dures specified i n SID Pro ce ss Specification MA 01 16-012.6. NOTES6. 1del ivered separate ly to the MSFC for ins t rumentat ion.will be delivered at a la te r date.

Delivery of Modules. - The SM, Adapter and In se rt will beThe LES an d CM

C.*.14

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JETTISON MOTORPITCH CON TRO L (LIVE)

LAUNCH ESCAPEMOTOR (SIMULATED)LAUNCH ESCAPE TOWER(SPACECRAFT STRUCTURE) COMM AND MODULEBOILERPLATEEXPLOSIVE BOLT SEPASYSTEM (SPACECRAFT)

SERVICE MODULERCS MODULES BOILERPLATE(SIMULATED) (ALUM1NUM )ADAPTER WITHAIRCONDITIONINGBARR1ER BO1LERPLATEINSTRUMENT UNITTEMP. CONTROL

S-IV STAGES - l STAGE

AS REQUIRED

Figure 1 . Boilerplate Number 26 Configuration

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APPENDIX ADRAWINGS

1 . Scope. - The following list const i tutes the top drawincomponents for Boi lerplate Number 26.

5 f m a j o r

NomenclatureGene ra l Assembly B P 26Genera l Assembly LES 15Body Group AssemblyTower AssemblyTower S t ruc tureSki r t As semblyPow er S ystem Instal la t ion, CompleteRocket Motor SetEle ct r ica l In s ta l la t ion, CompleteEle ct r ica l Instal la t ion, TowerWiring DiagramEle ct r ica l Instal la t ion, MotorGen eral Assembly, CM 26S t ruc t u re A ssem bly C o r~ p l e t e M 26S t ruc t u re A ssem blySt ru c tur e , Aft CrewAft BulkheadBulkhead - Forward AssemblyS t r u c t u r e - Aft Heat ShieldCove r Instal la t ion, Ablat iveEle ct r ica l Instal la t ion, CompleteElec t r i ca l Ins ta l la t ion , Crew Compar tmentWiring DiagramC over - SequencerEie c t r i ca1 In stallat on, Forward Compar tmentEle ct r ica l Instal la t ion Aft CompartmentGe ne ra l Assembly, SM 11St ru c tur e , Comple teS t ruc t u re , A ssem blySupport Assembly

NumberB14-000002-251B15-000002-221V15-300001-71V15-300100-11V15 - 3 001 02-241V15-300202-41B15-400001- 111B15-410001-41B15-450016B15-451401B15-45 0401B15-451410B16-000002-28 1316-300016B16-301006-401B16-311006B16-301081B 16-3 01 073-401B16-327006-91B16-320013B16-450016B16-451401B 16450430B16-451207-11B 16-45640 1B16-457401B17-000002-221B 17- 3 00026B17-320101B17-320140- 101

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Nomenclature

APPENDIX A (Continued)DRAWINGS

NumberFai r in g Ins ta l lat ion and AssemblyFa i r in g AssemblyElec tr ica l Ins ta l la tion, CompleteGeneral Assembly - Adapter 11Structure CompleteS t ruc tu re Inse r t

B17 -320 142B17-320141B17 -4500 16B18-000002-221B18-300016B18-320113

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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 . SPACE and I NFORM ATI ON SYST EM S DI VI SION

APPENDIX BPr oc es s Specif ica tions

1.Specifications for the Apollo Pro gr am ,fabr icat ion of Boilerplate Number 26 shall be as se t fo r th on the fac e ofthe boilerplate drawings.Specifications applicable to Boilerplate Number 26 .

Scope. - Section I const i tu tes a l i s t of approved General P ro ce ssThose p rocesses requ i red in theSection I1 constitutes the l ist of Specif ic Process

Section INumber NomenclatureAAOl 01 -004 Sem i-co ndu cto r, Ele ctri cal ly Insulated, Heat

Dissipating , Stud Mounted, Installat ion Pr oc ed ur efor

AAOlO6-020

AAOl08-005

AAOlO9 -0 12AA011O-002AAOll6-022

FA1-38

FA2 -101FA2-102

Sealing and Moisture Proofing of Gl ass and C era micComponents with Polydimethyle Siloxana FluidsApplication of Corro sion B a rr ie rs BetweenDiss imilar M e t a lGeneral Proced ure for Br ush Type Electropla tingSolvent Vapor Degr eas ingApplication of a Strippable Pr ote ctiv e Coating toPainted and Plastic SurfacesBonding of, Metal Honeycomb Sandwich P a r t s Usinga Vinyl Phenolic Adhesive i n Film F o r mSealing Electrical W i r e Bundles Passing ThroughBulkheads Subject to 400FEncapsulation of W ire Ha rn es s Junction for GroundHandling Equipment

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**+Pu..-'' - '

NumberFA 2 -103FA2-16

F A 2 -23FA2-90

FA6 -130

FA6-199FA6-2

FA6-236

FA6-91FA7-16

FA7 -17FA7 -34FA7-35FA7 -43

FA 7 -44

APPENDIX B (Continued)Nomenclature

Fu me Tight Seal ing of Ele ctr ica l W ire Bundles withNorm al Opera t ing T emp 275-350FFaying Surface Seal ing for A rea s wi th NormalOpera ting Temp era ture s f rom -65 to 2 2 FImpregnat ion of Cer ami c and Pla st ic PartsSeal ing Ele ct r ic Termin at ions, Subject toT e m p e r a t u r e s Up o 300FMachining of Aluminum Al loy Cast ing to Pr ec is eDimensionsIdentification of Teflon Insula ted C ableTurnb uckles Quick Disconnect Adjustment SafetyingP r o c e d u r eAttaching Sock ets to Wire Rope

Se am s and StitchingLaminat ing-Glas s Fa br ic and Non-Metall ic Sandwich,L o w P r e s s u r eFlat tened Tube EndsL am ina ti ng T e m pera t u re R es i s t ance Po l yes t e r R es i nFoam-In-Place P l as t i c Core Par t s Fabrica t ion ofLamin ating Epoxide Res in, Cold Curing, Non-S t ruc t u ra lLamin at ing Epoxide Resin, Heat Curing, Non-S t ruc t u ra l

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APPENDIX B (Continued)NumberFP5 -1 0

FP5-19

FP5-32

FP5-33FP5-34

HA0106 -040

HA0109-003HA0109-006

LA 0101-006LA0101-007

LAOl 01-009LAO101 -010

LAO102 -00 1

LA0102-002LAOl 02-00 3

- .: ,I

NomenclatureAppl icat ion of M oistu re and Fungus Res is tan tCoatingApplicat ion of Weather P ro te ct iv e Coating to RubberPartsPr ep ara t ion of Decalcomanias by the Si lk Sc re enP r o c e s sApplicat ion of Conv ersion Type Finish esCleaning Chemical F i lm Tre atme nt and Applicationof Org anic Coating to Integ ral Ta nksFum e Tight Sea ling fo r Area s with Norm al Opera t -i ng T em pera t u re s f rom 65 t o 27 5FAluminum Metal SprayingAnodizing of Magnesium Alloys DOW #17

Ins al lat ion of Bea rin gsBear ings S in te red Oi l Impregnated S torageMachining Pro ce ssi ng Instal la tionInstal lat ion of M etal V-SealsReceiving, Stor age and Instal lat ion of Dry FilmL ubr i ca inn C anponsn t sFab rica t ion of Detai l s for Res is tan ce WeldedCor rug ated Metal SandwichCold Straighten ing of St ee l Parts and Assembl i esElevated Tempera tur e Fa- ing of Titan ium andTitanium Alloys Non-Deliverable Parts

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N O R T H A M E R I C A N A V I A TI O N , I N C . SPACE and I NFORM ATION SY STEM S DI VI SION- - - l - n . * . e

NumberLAOl 02-004

LAOl 02-005

LAOlO2-006LAOl 02-007LAOl 02-009LA 0102 -01 0

L A0102 -0 11

LAOl02-015LA 0102 -019LA0102-024

LA0102-027

LA0103-001LAOl 03 -006L A O l 03 -010LAOl 03 -01 2LA 0 104 002

APPENDIX B (Continqed)

NomenclatureFabr icat ion of Detail P a r t s for Use in AdhesiveBonded Honeycomb SandwichFabr icati on of Details for B raz ed SandwichSt ruc u r eTitanium Alloy Forging sElevated Temp Forming of Magnesium AlloysLimi ta t ions fo r Pr ocess ing P H S tee l De ta i lsElevated Temp eratu re Form ing or StraighteningHigh Strength Aluminum AlloysCable Termina l Assemb l ies Fabr ica tion P r e -Stretching and Proof LoadingEleva ted Tempera tu re Forming of S t ee l P a r t sTest ing of Hose Assemb l iesStraightening of Braz ed and Heat Tre ate d PHl5-7M0Honeycomb Sandwich S tru ctu r eaSpr ings Compress ion , C lose ade ran ce , MFT andIn spec ion R equir eme ntsMachining of Close To ler anc e Sheet and Pla teThermal Cut t ingSurface Roughness and I r regul ar i t ie sDrilling of Ha rden ed AlloysMarking of Silicone Rubber Coated G l a s s F a b r i cElectrical Insulating Sleeving

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-4-.* -*

NCRTH A M E R I C A N A.Y!AT!ON. ! N C .

NumberLAOl04-003LAOl 04-005

LAO104-01 2LA0105-003

LA0105-012

LAOl 05-013

LA0106-007

LA0106-008

LAOl 06-009

LA0106-021LA0106-023

LAOl 07 -034

LA0106-065

APPENDIX B (Continued)

NomenclatureMarking of Parts and Assembl ie sU s e and Application of Fluid L ine S yste m Identifica-tion MarkingsApplication of DecalcomaniasFabr icat ion of Glas s F abr ic -Sil icone L amin ates forS t ruc tu ra l UseRoom Te mp era tur e Cementing and Laminat ing withMethyl M ethacryla te ResinPo s t Forming of Lam ina tes , Phenolic Shee t P las t i cMasking of Tr an spa ren t Pla s t i c MaterialsAdhesive Bonding of Aluminum Alloy Assembliesfor Usage a t -67 F to 180FAdhesive Bonding of Ther mos ett in g Pla sti c and Misc.Mate r ia l s for Usage from 67 to 180FAdhesive Bonding of Aluminum Alloy Assemblies forUsage at -67F to 260FAdhesive Bonding of The rmo sett in g Pl as ti cs and Misc.Mate r ia l s for Usage fro m 67 to 260FCementing Non-Structurai General Pur po seLiquid Tight Sealing of A re as with Norm alOperat ing Tem pera tu res f ro m -65 to 225FUse of R o o m Temperature Vulcanizing Sil icone RubberAdhe s veInsta l lat ion Pro ce du re s for 0-R ing Seal ing ofBo1 e d A s mblies

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NumberLA0106-072LA0106-098

LAOl 07 -001LAOl 07 -021

LAOl 07 -037LAO 108 002LA0108-030LA 0109-00 1LAOl09-004LA0109-005LAOl 09 -01 1LA0109-017LAOl09-021LAOl 11-001LAOl l l -006LAOl 11-007LAOl 11-008

APPENDIX B (Continued)Nomenclature

Use of Cold Curing Cataly zed Rubber Cem entAdhesive Bonding with Electrical ConductiveAdhesiveARC -Spot WeldingB raz i ng of High Tem per a tur e Nicke l BaseHoneycomb St ructure

Pe rc us si on Stud WeldingApplicat ion of W as h P r i m e rTeflon-TFE-Disper s ion Coat ing -725 F Fusio nApplicat ion of Sc ale Inhibiting CompoundApp licat ion of NA3 -1 373 Coat ing to Ti taniumNickel -Zinc Al loy P la t in gApplic ation o f A -418 Cer ami c Coat ingAnodizing and Coloring of Aluminum AlloysBlack Oxide F in i shes fo r SteelHeat T re atm en t of Aluminum AlloysHeat Tre atme nt of Carbon and Al loy Stee lsHea t Trea tme nt of Ti tanium Alloy Sheet and PlateH ea t T rea t m en t of Ti tan ium Alloy Bar Forg in gsand E x t ru s i ons

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NumberAPPENDIX B (Continued)

NomenclatureLAOl 11-009

LAOl 11-01 1L A O l l l - 0 1 2

LAOl l l -013LAOl 11-014

LAO11 .-01 5LAOl 11 01 6

LAO111-022

LAOl 11 023

LAOll l -024

LA0112-007

LAC1 15 00

LAOl 16-010

LAO11 -001

*

Pro ces s in g of Steel Par ts Heat Trea ted to HighTensile StrengthsHeat Treatment of Copper and Copper AlloysPos t -Forg ing Thermal Trea tm ent fo r U l t r a HighStrength SteelSt re ss Rel ieving of Titanium AlloysHea t Trea tm ent and Proces s ing of U l t r a HighStrength Steel AlloysHea t Trea tment of Nickel and Cobalt Ba se AlloysPrev entio n and Elimination of HydrogenEm br t l ement in S tee lHeat T reatm ent of Heat and Corro sion Resis tant ,Precipi ta t ion Hardening S teelsHea t Trea tment of the 400 S e r i e s C o r r o s io n R e s i s -tant SteelsHea t Trea tment of the Non-Hardenable, Austenitic ,Corrosion Resis tant SteelsApplication of High T em pe rat ure 650 F Solid DryFilm Lubricant CoatingAcceptance Standard for Br aze d Honeycomb SandwichPartsPre par ati on of NAA and C ustomer Industcial Equip.for Shipment and Storag eShot Pee ning of Me tallic Parts

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APPENDIX B (Continued)Numb erMAOlOl -001MA0101 -002

MA0101 -004MAOl 01 -005MAOlOl -006

MA0101 -007MA0102-001

MA01 02 -002MA0102-003MA0103 -001

MA0103-002MA0103 003MA01 03 -004MA0103-005MA01 03 -006

MAOl 03 -007

Nomencla tureInstal lat ion of In se r t s , Sc rew T hread , B rush T ypeInstal lat ion of Helical ly Coiled W i r e , ScrewT hread , In se r t sInstallation of Hose ClampsIns ta l la t ion of Threa ded and C ol lard Fa ste ne r8Ins al lat ions of Conventional Rivets an d BlindFas ener sInstal lat ion of Quick-Action FastenersFabrica t ion and Ins a l la t ion of Rigid and FlexibleTube Assemb l i esS tandard Detai ls fo r Meta l Shee t and Ext rus ionsInstal lat ion of Gam ah Flexible CouplingsC hem -Mi ll P roces s i ng of Stee l and Heat Res i s t an tAlloysCh emi cal Mil ling of Titanium and T itanium AlloysChem ical Mi ll ing of Aluminum Cast ing Al loysChem -Mil l Pr oc e s s i ng of Wrought Aluminum AlloysTol eran ces on Machined PartsChemica l Mi ll ing and Pro ces s ing of Welded Stainlee sStee l TubingElect r ical Discharge Machining

Y B -8SID 63 - 6 9 5


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NumberMAOl 04-001MAOlO4-002

MA01 04-003MA01 04-006MA01 04-008

MAOl 04-009MAOl04-OlQMA0104-011MA0104 -012MAO105-002

MAO105-003

MAOl 05-004

MA0105-009

MAO105-010

M A 105 -011

NomenclatureLe ro y Lettering of Instru men t & Control Panel sMarking Methods Using Po lye ste r PhotographicMater ia lMar king , Etch, Application ofFabr ication of M etal Foil NameplatesIdentification of Ae ros pac e G round Equipment Wiringfor NASA ProgramsMarkings, Stencilled, Application ofMarkings, Printe d, Application ofMarkings, Impr ession Stamp ApplicationD i r e c t M a r k h g of Production I temsEleva ted T empera tu re Res i s tan t Glass Fab r ic Phenol icLaminates Fabrication ofElevated-Temp -RES Glass Fa b-Phe n Lam inates forNon-Structural ApplicationsElevated Temp Resis tant , Glass F abr ic Reinforced,Phen olic Sandwich Cons tru ctio p, F a b o rPolyurethane Type Foam , Sem i -Rigid or Fiexibie,for Non -S truc ura1 ApplicationsLamina tes , Po lyes te r Res in Pr eimpr egnated GlassFab ric, High Strength, Fabri cation ofFab ric atio n of P la st ic Insu lation for WS-133AGuidance Body Section

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-7W

APPENDIX B (Continued)NumberMA0 105 026

MA01 05-031

MA0105-033MA0 10 5-034MA0105-036

MA0105-037MA0105-038

-0105-039

MA0 106-001MA0106-003MAO106-005

MA0106-008MA0 106 -0 10MA01 06-01 5

NomenclatureLamina tes Epoxy Res in Pre im preg na ted GlassFab r ic High Strength Fabr icat ion ofFabr ica tion Term ina l Boards f rom Glass -Reinforced P l as t i c Lamina teFabr icatio n of Flexible Poly ure tha ne Fo am InsertsSleeving Insulation, Extr uded Flexible, Dilationand Installation ofFabr icatio n and Installat ion of a Heat Trans fe rMedium for Use Between Electronics Modules andCold PlatesFoamed Res in Pr oc es s fo r S t ruc tu res Re inforcementand E lec t r i ca l Thermal , and Shock InsulationMicrobal lon Fi l led Explosive Absorb er Fabr icat ionofPhenol ic Lamina tes , E leva ted Tem pera t u re Res i s -tant , High Si l ica Fab r ic , S ruc tu ra l Fabr ica t ion ofSeal ing of Pre ssu r iz ed Fue l Com par tm ents fo rShort Te rm Service a t Temp Up to 400FBonding with Epoxy -Po lym ide A dhesiveAdhesive Bonding of Stee l and Aluminum Alloysfor Low Temp ServiceApplication of Metal Foil Namepl atesPotting of Connector Assemblies Using PolyurethaneGenera l Pur pos e Seal ing fo r A rea s wi th NormalOperat ing Temp F ro m -65 to 350F

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/

N 0 R T i - i A i v i E R i C A N AS! .AT!ON: I N C . SPACE and I NFORMATI ON S YSTE M S DI VI SI ONI I.,me-* -

APPENDIX B (Continued)Number NomenclatureMA0106-017 Aerodynamic Smoothing with Flexible Join t Fi l ter for

Serv ice Temps f rom -65 to 225FMA0 106 -01 9 Bonding Instrumentat ion with High TemperatureEpoxy AdhesiveMAOlO6-020 Bonding with Room T em pe ra tu re Vulcanizing Silicone

Rubber CompoundMA0 106 -022 Fab rica t ion of Adhesive Bonded As sy fo r U s e a t T e m p

from -310 to 200FMA0106-023 Bonding with Low Te mp era tur e Curing Adhesive for

Se rv i ce at -67 to 300FMAO106-024 Fabrication of Flu id P as sa ge Cooled, Adhesive

Bonded Metal to Meta l Assem bl i esSeal ing Window A re as wi th Low -Te mp erat ure Res is tan tRTV Sil icone Elast om er

MA01 06-026 Bonding with Low Pressure , 250F Curing Adhesivefor -67 to 200F Serv i ceMA0 106-027 Adhe sive Bonding C or k Com position Sheet for

Th erm al InsulationMA010 6 - 0 2 9 Casting Welded Electronic Modules in a Fi l led

Epoxy ResinMA01 06-031 Non-Structural Eonding with Low-TT-,~perat\lre-Resis

tant Si l icone RubberMA0106-032 Bonding with Low T em pe rat ur e Curing, Polyurethane

Adhesive for Cryogenic UsageMA0106-033 Bonding M etallic

St ructures for Cryogenic and Heat -Resis tantApplications

Meta l Com posite and Non -Metal l ic

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APPE NDIX B (Continued)NumberMAOlO7-001MA01 07 -002MAOl 07 -003MAOl07 -004MAO107-007

MAOl 07 -009MA0107-010

MA 0107 -011MA0107-012

MA0107 -0 13MA01 07-017MA0107 -0 18

MA0107-019MAOl 07 -020MA0107-023

MA0108-001

NomenclatureFus ion WeldingR e s s ance WeldingSi lver Al loy Br azingFu si on Welding of Ground Suppo rt Equipm entBraz ing of Aluminum

Tinning and Solder ing of Ele ctr ica l and Electr onicComponentsTinning and Solder ing of Ele ctr ica l and Elec tron icComponents fo r Aerospace Pro jec t sF u r n a c e B r a z in g of AM350 and AM355 C orr osi onR es s an t S tee l sInduction Brazing of 304L Cr es S tee l Tube F i t t ingto 304L C r e s & InconelBrazing, High Temperature , Above 1700FFu sio n Welding d Tube JointsSolder ing Aluminum, Ti tanium , and Steel forSeal ing Aerospac e Plumbing System sBrazing Aluminum to Co rrosi on Re sis tan t SteelPe rc us s i on Stud WeldingBraz ing and Hea t Trea t ing of PH Stee l HoneycombSandwich Str uct ure sProcedure for Polyurethane Coding of Elec t ron icCi rcu i t ry

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Number Nomenclature~ ~~

MA01 08-005MAO108-006-0108-008MAOl 08 -009MA0108-010MAOl 08-01 1MAOl 08 -01 3

Application of Organic F in i shes -Genera lP r im in g of Laminated and Moulded Plaatic SurfacesApplication of A c r y l i c Latex EnamelApplication of Epoxy -Polyamid P r i m e r Coat ingApplication of Asph alt Base Roof CoatingApplication of High-Build Vinyl CoatingAppl icatio n of Ai r Drying and Baking Epoxy-Amine Enamel

MA01 08-0 14M A 0 08 01 5

MA01 08-016

MA0108 -0 18

MAO108-019

MAOl 09-0003

MA01 9-002MAO109-003

Application of Stripp able Vinyl CoatingApplication of F r e e z e C oa ti ng t o W e l d e d ElectronicModulesApplication of Ozone a nd W e a t h e r Res is ta nt Coatingto Rubber PartsApplication of Chemically C ur ed Zinc Dust -Fil ledSilica te CoatingAppl ication of Pro pel lan t and Flame R e s i s t a n tMastic CoatingApplication of Chemical Fikn to Aluminurnand Aluminum AlloysPhos phate Coat ings for F e r r o u s M e ta lsApplication of Chemical Films to Aluminum andAluminum Alloys

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APPENDIX B (Continued)Number--MA0109-004MAOl 09 -005

MAO109-006MA01 09 -007MAOl 09 -008MAOl 09-009MA0109 -0 10MA01 09-01 1MA0109 -0 12MA01 10-001

MA01 10 01 0M A 0 1 0-011MA011 0 -0 12MA0110-013

MA01 10 -0 14

MAOl 10- 01 5MA0110-0 17

NomenclatureElec tr o l es Nickel Pla t in gRepa ir and Ref inishing of Abraded Scra tch edRework o r Cor roded Meta l Sur faceCadium Pla t ing Cyanide P ro ce ssCopper PlatingCadium Plat ing-F lu o bd r a te P r o c e ssChro mic Acid and Sulphuric Acid AnodizingHa rd Chr ominum Plat ingCold PlatingEle ctr ole ss Nickel Pla t ing of Aluminum TubingCleaning Fluid Sys . Tube Assemblies and Fi t t ing,Exc ept Liquid Oxygen and Liq uid HydrogenGe ner al Cleaning MethodsCleaning of Aluminum and Aluminum AlloysCleaning of Fe rr ou s AlloysCleaning and Pass iv at ion of Corr osion and HeatResi s tant Al loysCleaning and Pro tec t iv e Tre atme nt of MagnesiumAlloysCleaning Titanium and T itanium AlloysUltrasonic Cleaning

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APPENDIX B (Continued)NumberMA011 0-018

MA01 10-020MAOl 10-02 3MA0110-024

MA0 110 -02 6

MA01 10-027MA0111-001

K40111-002

MAOll l -003

MAOl 11-004

MA0111 005MA0112-002MA0 1 2-00 3MA0112-005

MA0 113 001

NomenclatureCleaning Components of Oxygen Syst ems a nd NitrogenTetro xide Sys tem sAbra sive CleaningStr ipping Organic Finish esSur face P repa ra t i on of Metals and Non-Metals forAdhesive BondingCleaning and Conditioning of Metals for Brazing andSo lde ri ng P roc es s e sF l ou re scent Pe ne t ra nt CleaningHeat Treatment of Fe r ro us and N on-Fe r rousAlloys -GeneralHeat Treatment of 17 -7PH Corr osion R esis tan tP r e s s u r e Tanks

Heat Trea tment of 17-7PH Steel Sheet to 170,000PSI Tensi le MinimumHeat Treatment of MB0160-003 Bar, ExtrusionsFor gin gs and MB0160-001 Pl at e 17-4PHHeat Treatment of 18NI Marging S tee lApplication of iv'loiybdenum Disillphide Coa tisg sApplication of Solid Dry Fi lm Lu brica ntApplication of Solid Dry Film Lubricant Coatingwith Top Coat Se ale rEle ctr ic al Bonding AS-1 Mi ssi l es

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APPENDIX B (Continued)Number NomenclatureMA0113-002MA0113-003MA0113 004

MA0113 - 005MA0113-006MA0113 -008MAOl 13 009

MA0113 01 1

MA0113 01 2

MAOl 1 3 0 13

MA0113 01 5

MAOl 15-00 1MA0115-005

MA0 115 -006

Ele ctr ica l Components and Hardw are , Mounting of ,Genera l Spec fo rTaper -Pins , Ins ta l la t ion and Te st ofWiring Ground Suppo rt Equipment Identification andInstallat ion ofShielded Wi re Ground Support Equipment Assem blyand Ins tallat ion ofBonding Ele ctr ica l Aerospac e Ground EquipmentTerm inal Crim p Style Aerospace Ground EquipmentInstallat ion ofCoaxia l Connec tors and Termi na l s , E lec t r i ca l ,Assembly ofInstallat ion of Aerosp ace Ground Equipment Wiringfor NASA Pr og ra m sMechanical and The rma l Str ipping of Insula tedHookup W i r eTermina t ion & Grounding of Shielded Wire inAerospace Ground Equipment for NASA ProjectsConnectors, E lec t r i ca l , Assembly and Ins ta l la t ionofUltrasonic InspectionTesting Compatibil i ty of Mater ia l fo r L iqu idOxygen Sys emIns ta l la t ion o f S t ra in Se nsor s

.. B-16SID 6 3 - 6 9 5

4%#F+Hk IA


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APPENDIX B (Continued)NumberMAOl 15-007

MAO115-008

MA01 15-009

MAOl 15-01 0MA011 5-01 1

h4AO115-014MA01 15-01 5MA0 116-01 2

MA01 16-01 3

MA0116-014

-h/T_AQ116-915MA 0116- 016

MAO116-017MA0116-021

NomenclatureTe st for Pr ef i t of Compomnts for Brazed HoneycombPane l sFlamma bil i ty Te st ing -Non-Metal lic Ma ter ials farManned Spac e cr af tAnalysis of Gassing Pro du cts fr om Non-Metal licMaterials in Manned Spacecr aft

Bondcheck Inspection of Brazed Honeycomb Panel8Identi f icat ion and Traceab i l i ty Requ irements forSup plier s of High Reliability P ar t s , Genera lSpecificat ion for NASA Pr o g ra m sScouring and He at Stabilization of D acronTest ing of Aerospace Plumbing Systems Detai lsPrep arat io n for Del ivery & Tr an sp or t of ApolloBoiler plat esIn-Plant and Inter -Plant Par t s Protect ionRequirementsSupplier Pa ckaging of Apollo S / M Main F ue l andOxidizer TanksClean Packaging Requireme nts and Pro ced ure sSupplier Packaging and Handling of High ReliabilityI t emsSupplier Packaging RequirementsAnti -Fric t ion Bea ring Supplier Packaging

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ncI r r + 4 h *,-Sb-nL

APPENDIX B (Continued)NumberMA01 16-027

MAO606-001

MAO606-002

MA0606-003MA 0606-004MA0606-005MAO606-006

MA0606-008MA0606 -009MA0607-001MA0607 -002

MA0607-003

MA0609 -002MA 0610 -004

NomenclatureI n t r a / In t e r P l a n t P a r t s P r o t e c t i o n R eq u i re m e n tsfor High Reliabil i ty I temsPot t ing Elec tr i ca l Wiring Tower Str uct ure ApolloLaunch Escape System Boi ler Pla te 12Bonding of W ire Ha rn es s, Apollo Launch Esca peMotor B /P No. 26Potting of Apollo Boilerp late Umbilical ConnectorPot t ing, Ele ctr ica l Wir ing, Apollo Launch EscapeTower S tru ct ur e/ Boi lerpla te No. 13 and SubsequentPotting of Umb ilical Disconnects Apollo BP LAdh esiv e Bonding, Apollo Comma nd Module HoneycombS t r u c tu r eBonding of Wiring Ha rn es s, Apollo Launch E sca peMotor B /P No, 12 and subsequentPotting of, C-Band Antenna CouplerSpot Brazing of Brazed Honeycomb SandwichFabr icat i on of Apollo Aluminum Cold Pl a t es byEu tec tic Diffusion BondingFusi on Welding of Tube Joint s for the Sat urn S-I1Ve h ic 1Co rro sio n Control of Apollo ComponentsCleanl iness R equirerrents for Apol lo Propuls ionS y s t e m s P r e s s u r i z in g S y s t em

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NumberMA061 0-012

MA0613-002MA061 5-001

MAO616-003

MBO 135 -01 2NAOlO8-006NA2 -41 85NA2 -41 94NA2 -7 147NA3 -01 10 1NA3 -01 52NA3 -0187NA3 -3756NA3 -51001NA3 -51 002NA3 -51 88PR10-8

W

APPENDIX B (Continued)

:SUP** ..-

NomenclatureCleanl iness Requi rement s for Apollo Spacec raf tCryogenic S torage Sys temEle ct r ica l Bonding for Apollo Space System a nd GSELeak Detection - Apollo Comm and Module Inn erSkin Se am Welding Join tsIn t ra / In t e r P lan t Par t s P r o ect ion R equ ire m n sfo r t he Apollo P r og ra mInsulat ion, Th er ma l , Fibro us, High Tem pCoating Emiss ivi ty Black, Appl icat ion ofPhenol i c Clas s Fa br i c Mol ded Par tsPoly es te r -1mpr egnated Glass F ibe r MatShee t and Plate Weldable Tita nium Alloy 5AI-2. 5SNDeoxidizer , Chem-Mil lAcid, Hydrofluoric TechnicalN i c k e l Sulfate H exahydrateTape, Masking, Chem-MillStr ipp er, Chem-lvi il i, Ti taniumMaskant , St r ippable , f or Steel Chem-MillS t r ip per , Chem-Mil lNAA Found ry Contr ol on Le ad and Lead AlloyCas t ings

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APPENDIX B (Continued)NumberPR3-6PR5-13PR5-14

PR5-15PR5-19PR5-20PR505-7PR507 - 3

PR7 -1 1P R 8 -1 0

PR9-10

RAOl 01 -003

RA0105-001RA0106-003

RA0106-006

RAO 10 9 -0 10

.&.

NomenclatureHard Nickel Pla t ingHea t Trea tment of Machining InvarStra ightening of Non-Corrosion Res is t ant SteelPar t s and Assembl iesHeat Trea tmen t of Gra y I ron Cast ingsStr etc h Aging of 17-7PH Stee lHeat Treat ment of 17-7PH Steel B ar s & Forg ingsS t re s s Relieving of Titanium AlloysHandl ing and Pro tec t ion o f Pr es su re Compar tmentSeal ing Surfa ceSta nda rds of Acceptance of Windshield G la ssClass i f ica t ion and Inspection Requirements forA i r c r a f t C a s t i ng sS t r e s s Relieving of T ran spa ren t Pl as t icEnclos u re sInse r t s and Studs Screw Thread Ke enser t ,Ins allat ion ofRigid Polyurethar s Fo am Application ofUse of Room Te mp C ured Contact Resin Adhesivefor Non-Structural P a r t sPot t ing, S i l i cone Rubber , Room-Temp C ure , E le c -t r i c a l S y s t e m sHand Anodizing A luminum Alloys

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co-

NumberSection I1

NomenclatureMA0201-0063MA0201-200

MA0201-0208MAO2Ol-0209MA0203-000 1

MB0203-0002

MA0 20.3-00 03

MA020 3-0004

MA020 3-0 028

MA0203-00 31

MA0 205 -0 0 11

MA0 205 -0 0 14

MA0205 0 039

Int e gra te d System Checkout P ro ce du reElect r ica l Systems Insula t ion, Resis tance &Continuity Check, Procedure forI&T Requirements - Intern al ApolloI&T Requ ireme nts, Subcontractor, SupplierEBW Fi ri ng Unit, LES Handling Installation &Checkout ofBa tt ery Stora ge, Silver Oxide Zinc M a r 4 0 9 0 ,Handling, Activation, Charging & Checkout ofBatter y, Storage, Silver Oxide Zinc, M ar 4 0 9 4 ,Handling, Activation, Char ging, and Checkout ofBat tery Storage, Silver Oxide Zinc Mar 4 0 9 5 ,Handling, Activation Charging & Checkout ofSA-7-BP: Apollo & Saturn E le c t r i ca l In te r faceCheckout Requirements forB / P 16 & 26, Relay Box, E lec tr ica l Pow er CheckoutProcedure f o rB / P 1 3 , 1 5, 1 6 , & 26: Sequencing Box, El ec tr ica lContr ol Functional Checkout & Calibra t ion Proce-dure fo rB / P 13, 15, 16 & 26: Tower Sequencer Assy.Control , Fl ight Worthiness Test , Procedure forModular Ele ctri cal Syste ms Continuity Check,Procedure f o r

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-%

Number Nome n cla ur e~~

MA02 10 00 05MA02 10 0 0 1 5MA0 302 -0 003

MA0 30 3-0 002

MA0303-0006

MA0 303-00 07

MA0 30 3 -0 0 15

MA0 30 3 -0 0 17

MA0 30 3-0 3 1MA0 303-032

MA0 30 3 -0 3 3MA0303-034MA0 303-035MA0304-0022

~ ~~

Launch Escape System - Assem bly and CheckoutLES , Th ru st Vector Alignment ofOrdnance Equipment Handling , Storage & Inspect ionP r o c e d u r eCable , Apollo Boilerplate Launch Escape Motor ,Looming ofColor Coding of E le ct ri ca l Connectors , P r o c e d u r efo rIdentific ation of W ire s , Cables 81 Connectorsfor Apollo Pro jec tMarking & Location of Elec t r i ca l & E l ec t r i ca lRefere nce Designators on Apol lo Spacecraft 81Boilerplate VehiclesPott ing of Relay Ass em blies using Polyurethane

Elec t r i ca l Wi r ing , Assembly & Installation ofEle ct r ica l Connector Assem bl ies , A ssembly ofE l ec t r i ca l Sys t em s Irs ulat iop, Resis tance &Cont inuity Check, Pr oc ed ur e forE l ec t r i ca l Wi re s & Connectors , Stowage ofCrim p Style Termin als El ect r ical CheckoutShielded Cable, F ab ric at i on ofPr oc ed ur e fo r Cal ibrat ion of Vibrat ion Mea surem entSys. Control Part - ME106-0015, ME411-0255,&ME 473-0036

B-22SID 63-695

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Number NomenclatureMA0 304-0 02 3

MA0 306 -0006

MA0 308-00 07MA0 308-00 14

MA0 309-00 14

MA0310-0001MA0 310-0002

MA0 310 -0004MA0 310 -0 0 05

MA0310-0006MA0 310 -00 11

MA0 311 0 0 0 4MA0401-0001MA040 5-00 02

Proced ure for Cal ib ra t ionControl P / N ME 449-0020

of L ine ar Acc e le r ome ter ,

Ins t al l at ion Pro ced ures for In t egra ted CoolingSystemAlignment & A ss em bly P r o c e h r eOrdnance Inst ' l . LES Tower t o Command ModuleSepara t ion Sys.Hardware E lec t r i ca l & Mec hanica l Mounting of0014Insulatio n of Buna-N R ub be r, L ET Application ofPr ote ct i ve Coating, Ozone and Weather R es i s t an t ,LES 81 C/M Applicat ion ofHandling, Inspection & St o rage of LESHandling, Inspection & Storage of Tower Je t t i sonMotorHandling, Inspection & Storage of PC MHandling, Inspection & Stor age of the Tow erJet t i s on MotorIns t al l at ion Proce dure fo r Insu lat ionDetect0 Temp Pain t and Tempi laq ApplicationB / P 1 3 , 15 , 16 & 26: Sequencing Box, E l ec t r i ca lContro l, F l igh t Wor th iness , Te s t Pro ced ure

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Material Specificat ions1. Scope. -Specificat ions fo r the Apol lo Prog ram . Those materials included i n theconstruct ion of Boilerplate Number 26 shall be a s se t fo r th on the face ofthe boi lerplate drawings.

The following con stitutes a list of approve d Ma teria l

NumberABOl 10-002ABOl 15-002

AB0120-001ABOl 20-007ABOl 20-009

ABOl 20-013

ABOl 25-002AB0125-004ABOl 25-010AB0!33-007AB0130-010AB0130-011

ABOl 30-013

NomenclatureCollant , Cor rosio n Inhibi t ingInsulat ing Materials , Elec t r i ca l Ceramic ,Blocks and ShapesSealant , CeramicResin, Liquid Polyamide , Thermoset t ingPoly sur ethane Compound Pott ing FlexibleNon-FlammableAdhesive Bonding and Sealing Compound, SingleComponent, S ilicone Rubbe r Ba seMagnesium Prote ct ive Tre atme nt DOW-17Cold PlatingCoating, Eopxy, Clear A i r DryingCoating Poiyur ethane Res in, FiexibieEopxy Resins Epichorhydrinbisphenol , Liquid TypeEpoxy Resin Epichlorohydrinbisphenol Liquid Type ,Gly cidyle ther ModifiedEopxy Compound, Filled, Sem i-Fle xible , SelfExtinguishing

, 0 ,* c 1SID 63 - 695


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APPENDIX C (Continued) /NumberAB0130-014

ABOl 30-01 6

ABOl 30 -021

AB0130-028AB0195-001AB0225-001AB0290-002HB017 0 -004LB0125-003

LBOl 25-004LB0125-101

LB0125-103LBOl 30-003LB0130-005LBOl 30-0 06LB0130-007

NomenclatureSilicone Rubber Low Tempera tu re Res i s tan t LowDurometer /5-15/Pottin g Compound, Silicone Ru bbe r, Room -Tem per atu r e -VulcanizingSi l icone Rubber , Room Temperatu re C uring/Durometer 40-55/Rubb er, Butyl SyntheticCushioning Ma ter i a l , Urethane, FlexibleCoat ing, Protect ive , Str ippableInk, Rubber Stamping/No n-Etching /Honeycomb Aluminum 5052 -H39, Mili tary Gra deChrominum Pla te Hard , Thin fo r Explosive Oper a-ting DevicesSi lver Pla t ing on Sta inless Stee l for Heat Ref lect ionSat in Finish on all A lloy P a r t s f o r A i r c r a f t I n t e ri o rT r i mHa rd Anodic CoatingsRubber , Natural , Low Temp Resis t ant 40-50 ShoreRes in -Prebodies Methy l Methrac ry la teRes n- Monomeric M ethyl M ethacr ylateResin-Low P re s su r e Laminating Self -Ext inguishing

c - 2 -IALSID 63-695


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4

APPENDIX C (Continued)NumberLB0130-008LB0130-009LB0130-105LBO130 -107LBOl 30 -1 13LB0130-114

LBOl 35-100LB0135-101LR0140-001LB0140-002

LBOl 50-001LBOl 60-100LBOl 60-1 1 3

LB0160-1 i7

LBOl 60-1 23

L BO1 60- 12 4

NomenclatureFabr ic , Dacron Heat Se t S t ruc tu ra l U s eFab r ic G lass , Acry l ic Res in ImpregnatedG l a s s Fabr ic , P re - Impreg na ted , S i li cone Res inRes in , Low Pr es su re Lamina t ing , High TempP o ly e s t e r B a s eRes in , Po lyes te r , G e l -CoatLamina ted Par t s Gel-Coated Glass -Fa br i cPo lyes te r Res inInsulation, Th erm al, Unbonded Gla ss Fiber BattT h r e a d , ClassCoating Solid Dry Film LubricantCoat ing Sol id Dry Fi l m Lu bricant , High Tem per a-tu re 7 00F MaximumBraided Tubing Asbestos Teflon ImpregnatedStee l , Sheet and Plate, PH17-5M0, CresAlloy and C r e s Steel , and Heat Resis t ant AlloyShapes TolerancesWelding Wire, Corrosion ar;d ?illederate HeatRes i s tan tSteel Ba r , Rod, & Shapes , 15-7M0, CorrosionResis tant , Precipi ta t ion HardeningMetals, Identification Marking

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APPEND IX C (Continued)Number Nomenclature

~

LB0160- 125

LB0160-126

LB0160-129LBO 160- 1 30

LB0160-142

LBOl 60-146

LBOl 60-1 47

LB0160- 148

LBO 160- 149

LB0160-151

LBOl 60-161LB0160-163

LB0160-165

LBOl 60-1 67

' :4*?Jl)(lr.

Close Tolerance S tee l Shee t & St r ip , PH15-7M0,Corro s ion Res i s t an t Prec ip i t a t ion HardeningStee l Tubing , PH15-7M0, Corro s ion Res i s t an tPrec ip i t a t ion HardeningSelec ted S t rength PH15-7M0 Stee l Shee t and P l a t eSe lec tor S trength, C lose Tolera nce PH15-7M0Steel Sheet & St r ipStee l Tubing , PH15-7M0 Corro s ion Res i s t an t , P r e -cipi tat ion Hard ening , WeldedCold Reduced and Te mp ered Hydr aul ic Steel Tubing350 Alloy Corros ion Res i s t an tSteel , 350 Al loy, Cor ros ion Re sis tan t Hydraul icTubingS t ee l Fo i l, C o r ros i on R es s an t, P rec i p i t a t ionHardeningPH 15-7M0 C or ros i on R es i s t an t S ee l Fo i l ,Condition 1 2 CS t e e l B a r , AIS1 Type 440C, Consumable Elect rodeVacuum MeltedSteel , E-2 AlloyDensi f ied Squa re Cel l s Honeycomb, PH15-7M 0C r e s S t e elS t ee l , Shee t S t r i p and P l a t e , PH 14-8M0, C or ros i onRes i s t an t , P rec ip i t a t ion HardeningC l os e T o l e r a n c e , P H l 4 - 8 M 0 St ee l Shee t, S t r i pand P l a t e T h ru 1 / 4 Inch

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APPENDIX C (Continued)Number NomenclatureLBO1 69-003 Nickel Strike Plat ing Te stLB0170-103 Sc re en , Monel MetalLB0170-105 Sterl ing-Lithium Br az e AlloyLB0170-110LB0170-113LB0170-122

Titanium Alloy GA1-4V Ba r and F org ingsTitanium Alloy S hee t , S t r ip and Plate GAL -4VTitanium Alloy /7A1-4MO/ Rod, B ar and Forgin gs

LBO170-124 Aluminum Alloy Sheet- Close Tole ran ceLBO 170-12 Aluminum Alloy, 7079-T6 & -T651, Sheet & PlateLBO 170- 126 Welding Wire-Titanium and Titanium AlloysLBO 170 - 130 Welding Wire- Corro sion and Heat Res is tant -Nick elBas e Al loysLBO 170- 138 Titanium Alloy/6A1-4V/ Clo sed Die Forgin gsLBO 170- 139LBO 17 J - 147

Titanium Alloy 7Ai-4M0 Closed Dye ForgingsTi tan ium Al loy /6A l /4V/Bars , Rods & ShapesExtruded

LBO 170 -160 Br az ing Alloy, Low The rm al Conductivity, 80/ 20Nickel M a t r i x

LBO 170- 163 Mag nesium Alloy She et, Close To ler an ceLBO 170- 167 Tubing, Corrosion & Heat Resis tant , NickelBas e Al loy/Rene 41/LBO 170- 169 Tubing, 2219 Aluminum Alloy

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* -

NumberAPPENDIX C (Continued)

Nomencla tureLBO170 - 180LBO 190-006LB0210-100LBO210 -10 1LB0210-109LB0225-100

~~~ ~

Sheet Lead 5-7'70 AntimonyTape Metal Foil , Fluid Line Identif icationB r a zing Stop -Off CompoundBright Dip Copper and Copper AlloysCle ane r E lect r o lytic AlkalineProt ec t iv e Coatings fo r Ti tan ium Alloys DuringHe at Tr e a tm e n t

LR0255-102

MBO 100-00 3

MBOllO-00 1MB0110-002MBO 110-003MB012-015

MBO 120-008MBO 120-0 19

MBO 120 -0 11MBO 120-01 3

Coating, Tim e and Temper a ture for Use onCadmium PlatingSubsti tution of T em pe r Con dit iq, Fo jrm , an d Sizefor Aluminum A lloysOxygen, Liquid and GasNitrogen, Liquid and GasHydrogen, Liquid and G asAdhesive , E leva ted Temp Res i s tan t , 300 t o 500LT Weight fo r Honeyc omb Sandwich ApplicationsAdhesive , Room Tem pera t u re Curing, S t ruc tu ra lAdhesive , Fi lm & P r i m er , fo r -310 to 200FUsageCompound, Sea ling, Gener al Pu rpo seAdhesive , Elevated Temp Resi s t a n t ,Lightweight

3 J 0 t 0 500F

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NomenclatureMBO 120-0 1 4

MBO 120-0 1 5

MB0120 -0 16

MB0120-017

MB0120-018

MB0120-020

MBO 120 -02 1

MB0120-022MBO 125-00 1MBO 125-002MBO 125-00 3-MB 12 5-0 0 5MBO 125-0 10MBO 125-0 11MB0125-012

Adhesive , Elevated Temp Resis tant 300 to 500 F ,Foaming TypeAdhesive, Elevated Temp Resis tant, 300 t o 500 LTWeight f o r Honeycomb Sandwich ApplicationsAdhesive , Tape Struct ural , fo r -67 o 200FServiceAdhesive, N i t r i l e Phenolic Film and P r i m e r , f o rMe tal to Metal Bonding 1-67 to 180F/Adhesive, for Bonding Vulcanized Neoprene toItself and to Dacron Fa br icAdhesive Structura l , Cryogenic, f or BondingMetal and Non-MetalsPolyurethane Compound, Potting and Coating,F exib e

Adhesive St ructu ral Cryogenic and Heat Resis tantSynthet ic Pro cess in g Lacqu er , Si lk Scree nCoating, PolyurethaneElectroless Nickel Pla tedCoating, Vinyl, High-BuildCoating, Zinc Dust -Fille d SilicateProte ctive Coating, Ozone and Weather Res ista ntEnam el, Epoxy-Amine, Air-Drying and Baking

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NomenclatureMBO 125-0 1 4MB0125-015MB0125-0 16MB0125-0 17MBO 125-0 19MBO 125-02 1

MBO 130 -0 01MB0130-004

MB0130-007M B0 130-0 11MBO 130 -01 2

MBOl30 -0 1 3MBOl30 -0 14

MBO 130-0 15

MBO13O-0 17MBO130-0 19

Bru sh Plate d Nickel and Tin on Ti tanium AlloyFreeze Coating Welded Electronic ModuleEna mel Gloss Rapid Air DryingEnamel , Alkyd, Semi-GlossCoating, Uretharie , Light DiffusingCoating, Zinc Dust Fi l led Sil ica Chemical lyCuredSil icone RubberGlass Fab r i c E leva ted Temp Res i s t an t , Phenoli cRe s in Pr eim pr egnat e dG l as s Fa b r i c , Po l yes t e r R es i n P re i m pregna t edMolding Compound, Phenolic Resin & G l a s s F i b e rFi l ledGlass Fab r i c , Epoxy Res in Impregnated , fo rSt ru ctura l Appl icat ions a t Temp Up to 300FFlexible Si licone Foa m, Room Tem p CuringCore , Honeycomb, Glass Fabr i c , Heat -Res i s t an t-423 to 500FLow Densi ty Rigid Foa m fo r T he rm al Insulat ion

Dacro n Cloth, Neoprene CoatedSil icone Rubber, Low T em pera t u re R es i s t an t ,Room Temperature Curing Durometer 55-65 '

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NomenclatureMB0130-022

MB0130-027MBO 130-028

MBO 130 0 32

MBO 130-033MBO 130 -0 34

MB0130-039

MBO 135-00 8MBO 135-0 1 0MBO 135-0 11MB0135-012MBOl35-013ME01 5-016MBO 150-00 5MBO 150-008

Rubber-Metall ic Gzsketin g, Oriented Mesh, fo rR F I ShieldingE la s to m e r , F u e l Re s i st a n t 7 1/2 DurometerElas tomers Space Environment R es s tan t 65 75Duromete rCasting Resin , Epoxy Type, Mineral Fi l ledSelf ExtinguishingInsulation Ablative Fil led Epoxy-PolyamideSi li cone Rubber , Pa s t e , Room Tempera tu reVulcanizingFoam, Po lyure thane , F lex ib le , Low Density 3lbs . cu . f t . Max.Glass Fabr ic , Scr imtypeInsula t ion ThermalInsulation Thermal MoldedIneulation Thermal Fibr ous High Tempera tu reInsula tion B lanket , Th erm alFi lm Aliiwlinized LMylar, Crin kle dCable, Ele ctr ica l , Shie lded and JacketedWire and Cable, Elec tr i ca l , Insulated, Copper ,600 Volts, =290 to /500

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APPENDIX C (Continued)NumberMBOl50-011

MBOl50-0 1 2

MBOl50 -01 3

MBO 150-0 14

MBOl50 -01 5MBOl50-017

MBOl50-018

MBO 150-0 1 9

MB0150-020MBO: 50-023MB0150-024MBOl60 -001MBO 16G-003

MBO 160-006

MBO 160-007

Id'*** . ,..Mi

Nomenclature-Wire and Cable , EleCtr ical Apollo Spacecra ft600 Volts, t o /250FWi re, Ele ct r ica l , Hook-Up, Shielded and Jack eted,600 Volt s 105C. Ma xim umWire , Ele ct r ica l , Hook-Up, Shielded and Jack eted,600 Volt -65 to 200C. Ma ximu mWire, Ele ct r ica l , Inter c onnection , Shielded andJack eted , 600 Volts , 105C. MaximumCable Flat Braided Ribbon 600-VoltW i r e , Thermocouple, Copper and Constantan,22 Gaugt St randed Fe p Teflon InsulatedW i r e , Thermocouple, Copper and Constantan,26 Gauge Solid F e p Teflon InsulatedCable, Miniature, Mult iple Conductor, 100p3 r cent Shie ldedCable , Elec t r i ca l , Spec ia l PurposeCable, Radio Freq uen cy, Coaxial , Semi-RigidCable, Radio Freq uen cy, Coaxial , FlexibleSteel , 17-4PH Cr es Plat e 170,000 Tensi le MinStee l , 17-4PH Corros ion Res i s t an t Bar s and Forg ings ,170,000 Tensi l e MinMaraging S tee l , Ba r , Ext rus ions , and Forg ings ,Prec ipi ta t io n Hardening / 18NI-9CO- 5MO-0. 5TI-0. 10AI/Tubing, Stee l Al loy, Corr osion Resis tant , Type 304L

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NumberMB0160-008MBO 160 -009

MBO 160 -0 11

MBOl60-0 12

MB0160-013

MB0160-014

MBO 160-01 5

MBO 160-0 18

MB0170-002MBO 170 -0 0 3

MBU170-008MB0170-010

MBOl70-011

APPENDIX C ( Continued)

NomenclatureWelding Rod and W ir e, Stee lBol ts and Screw s, Cor rosi on Resis tant , A-286AlloyHoneycomb, Welded, Pr ecip i tat io n Hardening,Corros ion Resis tant Steel Al loysLow Carbon Stee ls-B ars , Rods, Sheet , St r ip ,Pla te , Pipe Tubing, and ShapesSteel Cast ings, 17-4PH Al loy, Corro sion Resistant ,Precipi ta t ion HardeningWire , Spring Temp er , 17-7PH Corros ion Res i s t an tPrecipi ta t ion HardeningClose Tole ran ce, PH14 -8M0 , Vacuum InductionMel ted Steel Sheet, St r ip , and P la t e th ru 1 /2InchStee l , 17-4PH Corros ion Res i s t an t Bar Ext rus ions ,and Forgings for Opt imum Impact Prop er t i e sAluminum Alloy, 2014 Ba re Sheet and Pla teWeldable Hand Forgings, 2014-T452 AluminumAlloyStru ctura i Tubing , 6A1-4V Titanium Alloy WeldedWeldable Titanium Alloy, B a r s & Forg ings fo rApol lo Pressure Vesse l sFla sh Welded Rings, Fabricat ion Fo rm 2014Aluminum Extrude B ar o r Shapes

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APPENDIX C (Continued)Number NomenclatureMBO 170-0 12

MB0170-0 13MBO 170-0 14

MB0170-0 16MBO 170 -018

MBO 170-019

MBO 170 -020

MB0170-021MB0170-026

MBO 190-00 1MB02 10-00 1MB0210 -002MB0210-003

MB0210-004MB02 10-00 6

Inconel 718 Al loy , B ar , Forg ings and Forg ingStock, Consumable Elect ro de, Vacuum Mel tedSolder , Tin-Si lver Al loyGold-Copper-Nickel Br az e Alloy 81. 5AU-16.5AU-20. NIAluminum Alloy, 7079-T652 Hand Fo rg in gsStr uc tur al Tubing, $A1 4V Ti tanium Al loy,Ext ruded , fo r Apollo Launch Escape TowerGold-Nickel- Chrominum B ra ze Alloy, 72AU-22NI6CRTitanium Al loy/6A1-4V/ Fo rgi ng s for ApolloP r e s s u r e V ess el ComponentsAluminum Al loy, 2014 B ar e As-Rolled PlateInconel 718 A ll oy Fo rg i ngs , fo r P re s s u r e Vessels ,Consumable Elect r ode , Vacuum Mel tedN am ep l a t e s , Me t a l Fo i lChem-Mi ll P ro ces s in g , So lu tions fo rMixed Acid, Aluminum Deoxidized & EtchantTrichloro ethylene Re claimable Liquid OxygenCompatible

Cle an er , Alkal ine, Non- Co rro siv e, Low-FoamingF l uo re s cen t Pene t r an t In spect ion Ma t e r i a l s ,Oxidizing Agent Compatible

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NumberMB02 10 -007MB0210-008MB0225-00 1MB0225-002MB0290 -002

MBO295-004MB0295-00 5

MB0295-006MBO 95-0 0 7

wB0295-008MBOE95-009MB0295-010NBOllO-003RBO 130-00 5

RB0130-007

RBO140-002

APPENDIX C (Continued)Nomenclature

Water , High Puri tyClea ner , Alkal ine fo r Aluminum AlloysCoating, Vinyl, StrippageMas kant , Chem-Mill, Hand Strippab lePre c i s io n Clean Cer t if i ca tion Deca l Pr es su reSens it ive, Temp er ProofF i berb oard , Lam nat e d , C o r rug ate d Multi -P u r p osMater i a l C leanl iness Leve l P rec i s io n CleanPackagingFilm Transparen t , P rec i s ion Clean PackagingC l osu re s , Spec ia l P l a s t i c , P rec i s i on C l eanPa ckag ngTape, Non-Residual, Pr ec is i on Clean PackagingTef lon , Glass F i l l ed , Pr ec i s io n Clean PackagingParts Protect io n Mate rials and De