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SPACECRAFT EXTERIORCONFIG I,,'RATION

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ADAPTER STRUCTURE

RETRO.ROC KETSUPPORT BEÀMS

ENVIRONMENTAL C()NTNOL SYSTEI¡

COOLANT MODULE SUPPORT BEAMS

INTERFACE MATIHG LUG

(26 PLACES)

SHAPEO CHARGES

I'IDAC. ED93-36e68

CREW TRANSFEB

TUNNE L

EQUIPME NT

BEAM

BLAST SHIELD(REF E RENC E)

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HEAT PROTECTIONBE BYLLIUM RETÀIN E B

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STRUCTURAL DETAILS

B EAOE O REI{E SHIXGLES

TYPICAL SUPPORT FOiì BERYLLIUM SH.INGLES

HO^C aE'2l -¡6968

FI BERGLASS CHAH II EL

IHSULATION

r Nsu LATl0l{

TYPICAL SUPPORT FOR RENE SHINGLES

REI{E SH IH GL ES

FIBERGLASSCHANNEL

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cEAtNl B Moac.EE203 -36908

RE-EIITRY COHT RO L SY STEM

PABACHUTE

INTERIOR ARRANGEMENTBLAST SH IE LD

CR EIT TBÂìISFER TUHT{ EL_

I ¡ISTRUM EH TS AHO OISPL AYS

TBAHSFEB EOUIPM E HT STOYIAGE

PILOT & OROGUEPA RAC Ht' TES

H EAT SHIELO H ATC [ILPB HATCH

PAD ABORT CONTROL SYSTEÍ

aTTITU DE COHTB0L EqU IPH EilT.

EII VIROHÀtE HTA L COHTROL SYSTEM

RE-EHTRY TTOD UL E

RETRO ROCKETS..----J I --:I

COOLA HT PUMP MO OUL EI

TH ERMA L C URTAIIIsE PARATr0lr SPR tXc (TYP)

ELECTRICAL IIITERFAC E

h\z\-nÞrïrx.+É

1

INSTRUMENTSAND DISTRIBU

RE.ENTRYCONTROL

(GP- 4)

GEMINI B INBOARD PROFILE

RECOVERYPARACHUTE

RECOVERY

CREW TRANSFER TUNNELUMBILICAL & PBHATCH STOWAGE

SECTION

DATA STORAGE RH

HEAT.SHIELD HATCH

PB HATCHDATA-RETURNSTORAGE BOX

PROPAND LH FOOTWELL

M-39474

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FIGURE I-I

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GEIAINI B

COMMUNICATION SYSTEM

@ necove nv BEAcoN O c-BAND PowER DlvlDER

@ xr votcr r/n @ eHasr SHIFTER PowER SUPPLY

@ c-anruornaNsPoNDER @ c-oaruo ANTENNAS (3)

O vHF vorcE T/R (2) @ Hr wHte ANTENNA

O c-BAND PHAsE sHIFTEß @ volcr coNTRoL CENTER

@ ouaontelrxrn

@coax swrTcH (3)

@ oescrrur ANTENNA

(D RECOVERY ANTENNA

@ ruosr sTUB ANTENNA

@ vHF TETEMETRY xMTR (GBo oNtY)

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PROPULSION SUBSYSTEMS

RE.ENTRY CONTROL SYST

HC'AC . CE'r4ó -369G6

RETROROCKET(TYP ó PLACES)

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ENVIRONMENTAL CONTROL 5YsTEM

COOTING WATER TANK

POWER SUPPLIES -.'''"':-^ --' a-<. (

\,-'-\,/\ ,1 ,,,--\?

ENVIRONMENTAT CONTROL SUIT_ SUBSYSTEM

ENVIRONMENIAL CONTROL

COOIING MOOULE

PRIMARY OXYGENSUBSYSTEM

GUIDAHCE COMPARATORINDICATOR

ATTITUDE DISPLAY

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GUIDANCE AND CONTROL

INDICATOR

FLIGHT OIRECTOR

MANUAT DAÌAKEYIOARD UNIT

MANUAL DA]AREAOOUT UNII

INDICATOR

EUCIRONIC TIMER

ATNTUDE DISPI.AY

AUXILIARY IAPEME MORY-

EVENI NMER

INCREMENTAIvEtocllY

INDICATOR

INDICA

TI,JGHT CONTROI

l,l'r'.C. ET'l!5-369G8

UIDANCE INIERFACEADAPIEN

GIMBAL CONTIOT TTECTIONICS ISTATIC POWTI SUP?IY

INERIIAT PLAITOIM

L sYsfEM ELEcTRoNlc5

PAD'ABORI THTUSIET TTECTTONICS

At COMTUTER

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ELECTRICAL SYSTEM

O squta BATTERIES

@ uarx BATTERIES

@ sxuxrs

@ u¡a PonER otooE PANEL

@ uatn PowER PANEL

@ sus-aus FTLTER PAIIEL

@ tnlenrlce coxNEcroR PAIIEL

@ nelav pANELS

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AUXILIARY HÂIIOLE - SIOITEOROTÂIE TO USE.(jr E aT sH tELD HÀTCH 0r.{LY)

c0l{TR0LH AIIDLÊ

c0M8H ED LtECI{ANtCALIIIDEX TAB & I{AIIl¡LE

STOWA GE ERACKET

PRESSUB E EqUA LIZ AT IOH

VALVE - PB HATCH ONLY

LARGE PRESSURE BULKHEAD HATCH

H EAT SH IE LO HÂTCH

TYPICAL ÊXCEFT AS ilOTED

LX

INT Eß LOCX

HAII OLE STOWAGE ESACKET

v tsua L THDEX A|DS (3)

HÊAT SHIELD HÀTCII

INSTALLEt¡

CREW TRANSFERHATCH ES

BUNGEE CONO - \\

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FORYIABD PAI{ E LSTOI{ABLE ABEA

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SYSTEM ACTIVATIO¡I

HATCH

ACTU AT O R

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MAN U AL

FIRIH G

MECHANISM

CATÀPULT FIBES

LANYARDS PULLEO

MILD DET()NATING

FUSE LINES

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SEAT - MÀN SEPARATEO

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ISOO LB BREAK LINE

RECOVERY MODULE

BAG HÂNDLES

OEPLOYMENT BAG

MAIN PARACHUTE

DEPLOYMENT PROCESS

þtoac . ED

MAIN CHUTE

RISER

SINGLE POIN'f

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CHANISMIE

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DOCKING M

PE CAPSULI

LABORATORY VEHICLEDOUBLE MOL

ESCA

EVA AIRLOCK

STATION'S OPERATIONS

EXPERIMENTBEAM

CONFIDENTIAL

WATERSUPPL

MISSION MODULE

EXPERIMENTHANDLING BOOM

UNPRESSURIZEDCOMPARTM ENT

CONFIDENTIAL

XPERIMEN

ATMOSPHERE

A IR LOCK

PRESSURIZEDIOMPARTMEN'

SUPPLIES

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CONFIDENTIAL

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AIRLOCK

DOUBLE MOLSUPPORT VEHICLE

REPRESSURIZATION TANKS

CRYOGENIC NITROGEN

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CRYOGENIC OXYGEN

PRESS COMPARTMENT

SEPARATION PLANE

ASTRONOMICALT E LESCO PE

WATER SUPPLY

MISSION MODULE

CREW QUARTERS

M-40813

PRIVATE QUARTERS

HYGIENE COMPT

COMPARTMENTUNPRESS GEMINI B

CONFIDENTIAL

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INSTRUMENTATION COM PONENTPCM ÃE COR D ER

SPL AMP LIFIE RS

sPL MtC R0 P 0t{ ES

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TNSTALLATTONS . cBQ "'""

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rr{STRUMENTATION COMPoNENT INSTALLATIONS' GBQPCM RE COR OE ß

SPL AI¡P LIFIT, RS

SPL MIC ROPI{ OX ES

ILLUMIIIATION LIGH T

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REFERENCE

JUIICTI()N

L OfI LÉVELCOMM UTAI OB

MOL LABORATORY I\/1ODULE INBOARD PROFILE

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llillozos

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FIGURE IL

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Inte¡costals are provided, as required' between f¡arnes for the support of

equiprnent'Thecorrugationthicknessis0.lZ5in.inadiarnondshapedpattern at the hardpoint.s and tapers to 0.050 in. rnidway between hardpoints.

The corrugation thickness at each intercostal is selected to rnatch the load

that lntercos tal rnust dist¡it¡ute'

The aft end of the MM is sealed ott *itf, a flat diaphragtt *ti.tt is provided to

control the pressure bleeddown rate during boost. The diaphragrn is fabri-

cated frorn 0.080-in. 7015-t6 alurninurn which is chern-rnilled to 0.020 in.

away {rorn the edge attachrnent. The rnaxirnurn p¡essure differential ac¡oss

the diaphragrn is 3 psi. This pressure differential bows the'diaphragrn

4.0gin.forwardintotheMM'ThernaxirnumPreSsuredifferentialintheaft di¡ection is 0. Z psi and the ¡esultant bow is I' 82 in'

f,

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Section 7

MISSION MODULE

The MM (Figure 7-I) is 37 ft long' It is built in two sections which are

joined with a bolted fietd splice' The forward section is l4-lfZ ft long and

the aft section is ZZ-IlZ ft long. Each section is rnade up of eight corrugated

panels. The diarneter to the inside su¡face of the corrugations is l0 ft'

There are lZ0 corrugations around the circurnference' With the lZ0-in'

diam, the corrugation pitch is thus I ' 57 in'

The corrugated panels are biake forrrred frorn ?0?5-0 alurninurn which is heat

tleatedandagedtoTOT5-t6aftel.forrning.Sheetingl/Bin't}rickisusedforboth the forward and aft sections so thät the sarne brake die can be used'

The panels run the full Iength of each section' They are taper che"m-rnilled'

The chern-rnilled thickness in the fo¡ward section tapers frorn 0' 031-in' at

the front end of the forward section, where the design cornpressive load is

1,23O lblrt'., to 0. 038 i-n' at the aft end of the forward section' where the

designcornpressiveloadis],86zlb/in.Theche¡n-rnilledthiclalessintheaft section tapers frort 0. 038 to 0. 050 in'

The MM is joined to the Titan at eight hardpoints' Four of the hardpoints

are localed at + 33' frorn the MOL Y-Y axis' The other four hard points

are located at* ?Z'I lz 'Lr orn the F-F axis' Eight explosive nuts are initi-

ated to seParate MOL frorn the booster. The panel splices are located rnid-

way between hardpoints so that four panels are 40-1 /Z' wide and four panels

are 49-1 /2" wíde, or 42.5 and5l'pin., respectively, between spLice

c ente r line s .

Twenty-seven frarnes, including the frarne at the aft seParation joint' are

used in the MM. The larges u separation belween frarnes is I8 in' , and the

srnallest separation is 15,2 in. The frarne at the separation point is 8-l/Z in'

deep. The frarne Z bays frorn the aft end and the frame 7 bays from the aft

end are troth ?-1/Z in. deep. The rernarning 24 frarnes are aLl 3 in' deep or

les s.

3l

MD

RADIATOR FRAME BUMPER SUPPORTS

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RADIAL FRAMEBUMPER LOCAT ION

BUMPER SUPPORTS

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SILICONE RUBBER

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RADIATOR SYSTEM

..-SUPERINSULATI0N

SON SILICONE SPONGTRU BBER

FIGURE 5-24

ING LAYOUTEM - PLUMBI

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FORWARD

MAN IFOLD

ST

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RADIATOR SY

OVER TUBES F

FIGURE 5-27

AFI

MAN IFOLD

F}VD

RAD IATOR SYSTIM - FORWARD MAN IFOLD LEFI-S IDE RAD IATOR

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FIGURE 5-28

BIRDCAGE--LOOKING AFT

FIGURE 5 -IO

RADIATOR AND METEOROID SHIELD

MYLAR SHEETS

.016 ALUM6061

INSULATION

FIBERGLAS

.032 TITANIUMCOMM PURE9046 TYPE I COMPOSITION B

CONDITION ANNEALED7O,OOO PSI YIELD

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SILICONE RUBBER

.020-7075ALUM

M-39379

ALUM

45"SEG

7075-.O32ALUMRETAINER

45" SEGMENT

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ALUM6063 EXTRUSION

ME'IEORO I D SH IELD - NONRAD IATOR SEGMENTS

HORIZON SENSORFAIRING .Oó TI

HATCH

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ls\ --.,- .').'..-

r--.-r ,-r r-r t-r r-t r-r r-'!t F l li+l icf,l lFr Él

- ALUM EXTRUSION

BOTTOM PANEL

TOPPANEL SILICONE RUBBER

.032 - 7075ALUM

ALUM

F¡GURE 5-I9