LUNAR EXPEDITION PLAN

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4.2.3 I2FE SUPPORT 4.2.3-1 The life support package for the Manned lunar Rtyload vLll be required to function for a "ilplitniw of 10 days* Bile is based on the premise that a one-nay trip to the noon will require 2^ days, and the stay on the lunar surface will be on the order of 5 days. Die life support system must be capable of supporting three men during high acceleration boost, approximately 2i dayB of weightlessness, one to five days of l/6 earth weight, 2f days of Weightlessness, re-entry deceleration and return to full earth gravity- At the sane tine it mist provide a shirtsleeve cabin environment under the space and lunar environments, including extreme temperature gradients, absence of oxygen, radiation, etc. 4.2.3-2 Studies of the life support system weight requirements indicate that the life support package can be provided within the weight allocation for the 20,000 pound Lunex Be-entxy Vehicle. She life support system weight analysis was based on physiological experiments under simulated space flight conditions such as confinement, special diets, reduced pressure, etc At the present time approximately 65 to 70 percent of the knowledge required to design the three man package is available. However, to obtain the additional data experimental laboratory and flight testing is required. Most information is presently obtained by piggyback testing aboard experimental vehicles but to support the lunex program and to meet the desired schedules the BOSS primate program must be initiated and adequately supported. 4.2.3-3 Most of the data available today consists of physiological support (nutrition, breathing oxygen, pressure suits, and restraints for limited periods), but there is a lack of knowledge on prolonged weightlessness and the biological effects of exposure to prolonged space radiations. One BOSS program initially will support a chlmpanxee for periods up to 15 days and has been programed to provide a life support package of sufficient else and sophistication to support a man. Ems, with the BOSS^xrogram the data will become available so that the Lunex program can design and construct the life support package as required for April ^965^ 4-17 VDLAR-S-458 TOi tftc«M«i> (MIoiH kiloiMMiwi B#«t!n* DM •rfoaai M M W at At United Stain wMia *• naaaNii at iht IipwnK Uwj, TIN* If. U.S.C.. Sta-* 7W and 7M, *• tromnjiilon or rayafetiM at vkicli li any mammr M aa *aatHmttti *•»•» (• mbitotrd »i tow.
4.2.3.4 > atfti'3 m Shroaghout this development all life support knowledge and techniques will be fully exploited. Techniques, learned In the work with the Discoverer package were utilized in building the Mercury package. In turn, experience end knowledge gained from Mercury is being fully exploited in the development of the present BOSS package, 4.2.3-5 The life support program (BOSS) is vital to meet the objections of the lunex program. However, other AFSC programs bust be considered for possible application to Lunex and the following are nov being evaluated: 6373 (0) Aerospace life Support 7930 (U) Bib-Astronautics 4,18 KDLAR-S-458 4 f*H Tkh rfacniMt imttlftt informed*! •Madia* tka mtlml M m o* rtu United Stain wJfhtfl Ha nadniM •* M» Up\mof (CM, VUm •I. UJS.C. SMIWI 7*3 wirf 7W. Ha tratnmlnifm «r mftOttm af •h;iWM tar !•».•
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.. . 92 LUNAR EXPEDITION HEADQUARTE
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GENERAL LUNAR DATA Dlitont* hoiii n
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DOWNGRADED AT 12 YEAR INTERVALS: MO
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••-a- INDEX + * n3--& TITLE PAG
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CTSf £:* 43 --at an earlier date a
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in 1965.
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1 FROORAM tamau IB J LUNAR EXPEDITI
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SECTION II PROGRAM BESCRIFTIOH LUHA
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INDEX*- -"-*•••• *r--> •*
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two payloads in comparison with oth
Page 21 and 22: any unmanned BystemT It Is veil rec
Page 23 and 24: SfiGftcT Abort capability during Ea
Page 25 and 26: m !---* iflt «a«.[H^.>'' scale, a
Page 27: muj tVW U
Page 30 and 31: SECTIOK III MASTER ECHEDUIES LDNAR
Page 32 and 33: TITLE RAGE *- 3.1 RECORD CF CHANGES
Page 34 and 35: sww CONHLtLlV'llAL. 3-2 " LUNAR EXP
Page 36 and 37: • & • .* 3.6 PERSONNEL ^r AND 1
Page 38 and 39: • k- . *-, ^ CY IS CY* C Vi'ONDJF
Page 40 and 41: pf 4 _-$» AL
Page 42 and 43: PKMIAM KHNU - 6 Years **»?. m D LU
Page 44 and 45: MOOtAM SCHBUU - 6 Years TTT TJ (Con
Page 46 and 47: '**%' 8S*-S-HV r ia.W.
Page 48 and 49: i i-fli'- IHJI.I- 1 n fi "3a. as^-s
Page 50 and 51: - 6 Years IIT-F j LUNEX CIVIL ENGIN
Page 52 and 53: CY-66 CY -67 CY-6C JFfllNJJlSONDJFM
Page 54 and 55: ssf-s-svnaA .1 _ ijH ,-, w-« £9-A
Page 56 and 57: CHANGE NO. T .RECORD OP CHANGES INS
Page 58 and 59: **i*$& i v-' - •*-:. '.J. * * ***
Page 60 and 61: fc.1.2 MANNED LUNAR PAYLOAD *V -9 T
Page 62 and 63: ( -«H : - The lunar launching Stag
Page 64 and 65: S^*P £z k.2 SUBSYSTEM BEVELOFMEHT
Page 66 and 67: of selected vehicle configurations
Page 68 and 69: li.2 1.3A DYNAMICS ^iia^djajj^fi' (
Page 70 and 71: 4.2.2 HIOFULSIOH 4.2,2.1 cdia -•
Page 74 and 75: 4.2.4 FLIGHT VEHICIB ?OWEfi 4.2.4.1
Page 76 and 77: will be attainable. Also, no diffic
Page 78 and 79: 50899 (u) Molecular Amplification T
Page 80 and 81: 1 rrttjiMiinrirnii uuui nfemmf b. F
Page 82 and 83: 4.2.8 EWIROHMEimL DATA 4.2.6.1 ft-e
Page 84 and 85: •** tWKfltWTlAIr In order to dete
Page 87 and 88: A^wt; 4.2.9 MATERIALS ^!C» w 4.2-9
Page 89 and 90: k-3 TEST PLAN
Page 91 and 92: «**& 2heee tests vill provide data
Page 93 and 94: «,..*.» vMln *• mmlng of iha fi
Page 95 and 96: difficult step. Jhe major testing s
Page 97 and 98: a. Evaluate the effects of engine b
Page 99 and 100: k.h mODJCTim PLAff **i '**^4 At the
Page 101 and 102: I. . FKOHE 4-3 ' i GENERAL ARRANGEM
Page 103 and 104: "7 *"4C'" "-?•• FIGURE lf-1 MAH
Page 105 and 106: S3CTIC5I V BODGST /JH) FIHAI7CIAL L
Page 107 and 108: INBEX ***•••*: ;2* TITLE PAGE
Page 109 and 110: **!-
Page 111 and 112: 5-3 FY 62, 63 FINANCIAL PLAN MANNED
Page 113 and 114: EECTIOH VI PROGRAM MANAGEMENT LUNAR
Page 115 and 116: INDEX TITLE PAGE .- 6.1 RECORD OP C
Page 117 and 118: 6. ' HUX3RAM MANAGEMENT 6.0 MANAGEM
Page 119 and 120: V"? personnel within the Rrogram Of
Page 121 and 122: *SJffi c and sequence of events are
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I I MATERIALS | vunrraoffifiL
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SECTION VH MATERIEL SUPPORT IHNAR E
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nnsx «**'.w-i -***. TITLE PAGE 7.1
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7- MATERIEL SUPPORT 7.0 IHTflODUCTI
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d. Control of repalr-overhaul-modlf
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^_ ,(,OlW-i Certain Items, such as
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d. Altitude Simulation Unit - - A p
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£•.:. • • • •- As --r*;
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8.1 LUHAR LAUNCH COMPLEX The Lunar
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environment simultaneously with the
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CONFIDENTIAL *"- 'WWW' WDLAR-S-458
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»MHBfiimfc I'-V-Iwf^,,,.,.,^... .
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CHANGE NO. RECORD OF CHANGES . IESC
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«*w **•*-«, •*!:. • • * *
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; £.*. te^Ltj^r&& Personnel *(Spac
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'~*3!-.,..,..•-..... ;X*) ^ype IV
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^^s^*f3C^^ L SB6BS .*v^| • e. Qua
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ii msr' -fe*fc (2) flight test oper
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- "-^m, (2) Training films and tran
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I*-? 1 ^ ;: f ,i * Proposed «* Num
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? Major Segment of System Vehicle S
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I. ••- ' ttr»*M*w CHABT EC - B
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mmjmmmMumammmt sk-.-^^:-/: ^;:-S" :
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.; -.
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i ssvs-innaM 3 r r • n 99 A3 I V
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CY 63 CY 64 CY 65 CY 66 £ i i J F
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BT CV 62 CV 63 Ct 6h 23 2S J I A S
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~?t. rW---^=t.-.i?^..-- . .J-: ,> n
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jspjiyjziffli^^ ASSESSMENT ASSESSME
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NAR RAYLOAD WDLAR-S-458 ON-LAUNCHER
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CHANGE NO. i t. RECORD OP CHANGSS D
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Site 1 - •T'Z • This page inten
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pound thrust. The estimated tine fo
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V Actual accomplishment of the proj
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c MANNED 'LUNAR PAYLOAD cam LUNAR R
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; - = * f t - •*TTF «... s.'. \
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__?_. ***** (JUBMFU u.'i -* __ ^ ^
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tf *SS- TTAT Lunar Chart • . , ;
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LUNAR EXPEDITION PLAN

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