LUNAR EXPEDITION PLAN

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...*:, •*P : -J&3, TITLE PAGE RECORD OF CHANGES IKDEX 8.0 nnRonjcnoN 8.1 <strong>LUNAR</strong> LAUNCH COMPLEX 8.2 LOGISTICS HJIEX 8.3 AEROSPACE GROUND EKVIBOHMEBT 8.3 v~--'- *• '«'.'**• 8.1 8.3 8.5 8.6 8.7 8-7 WDIAR-SA58 hi. decnml csMahn hfomatioit eHecHni tfe* natiaMl
d. Altitude Simulation Unit - - A plenum chamber, containing steam jets up stream of its exhaust bell, shall be attached to each engine for altitude simulation. e. flame Deflector - - The design is a conventional configuration elbow shaped, shield cooled with a firex water injection system. f. Propellent Storage and Handling Equipment - - A central LOg storage and transfer facility shall be provided for each of the two test facilities. The Lunar Landing Stage facility shall store 350,000 lbs. of LQa- Spherical, vacuum Insulated devars shall be used. Ihe transfer unit shall be a motor operated centrifugal pump vith 500 gpm and 100 psi discharge head capacity. Die lunar launch Stage Vest facility LCU storage shall contain 18,000 gallons in spherical devars vith a transfer pump capability of 200 gpm and 100 psi discbarge head. Distribution lines for both complexes would be prefabricated, static vacuum, insulated steel pipe. An LHjj storage and transfer facility will be provided at each hot firing test stand and the cold flow test pad. One transfer system Is an LHg gas generator system vith air being the thermal source. Pressuring level in each tank would be 100_ psi. The LH2 storage capacity requirement for each lunar Launch Stage facility is. 15,000 lbs. and at each Landing Stage Site is 35#000 lbs. Again the storage facilities would be spherical devars vith segmented, prefabricated, static vacuum insulated stainless steel pipe distribution lines. •fcrr**,* WDLAR-S-kjS Tfcli rfacmnl EWHaIn lufarairtloa aHactfai Dm notlanal M M H at Ik* UaiMd ftotw within tin maafilat. at tfca fealaaaart lam, TWa II, U.i.C, lactiaa 7*3 and 7*4, Ifca hamtilMlm w lanlaHaa at whkli In an* «•)•« l» «a •muHnrlMd panan l> anMbHad »r lav,
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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
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any unmanned BystemT It Is veil rec
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SfiGftcT Abort capability during Ea
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m !---* iflt «a«.[H^.>'' scale, a
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muj tVW U
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SECTIOK III MASTER ECHEDUIES LDNAR
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TITLE RAGE *- 3.1 RECORD CF CHANGES
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sww CONHLtLlV'llAL. 3-2 " LUNAR EXP
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• & • .* 3.6 PERSONNEL ^r AND 1
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• k- . *-, ^ CY IS CY* C Vi'ONDJF
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pf 4 _-$» AL
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PKMIAM KHNU - 6 Years **»?. m D LU
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MOOtAM SCHBUU - 6 Years TTT TJ (Con
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'**%' 8S*-S-HV r ia.W.
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i i-fli'- IHJI.I- 1 n fi "3a. as^-s
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- 6 Years IIT-F j LUNEX CIVIL ENGIN
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CY-66 CY -67 CY-6C JFfllNJJlSONDJFM
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ssf-s-svnaA .1 _ ijH ,-, w-« £9-A
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CHANGE NO. T .RECORD OP CHANGES INS
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**i*$& i v-' - •*-:. '.J. * * ***
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fc.1.2 MANNED LUNAR PAYLOAD *V -9 T
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( -«H : - The lunar launching Stag
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S^*P £z k.2 SUBSYSTEM BEVELOFMEHT
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of selected vehicle configurations
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li.2 1.3A DYNAMICS ^iia^djajj^fi' (
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4.2.2 HIOFULSIOH 4.2,2.1 cdia -•
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4.2.3 I2FE SUPPORT 4.2.3-1 The life
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4.2.4 FLIGHT VEHICIB ?OWEfi 4.2.4.1
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will be attainable. Also, no diffic
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50899 (u) Molecular Amplification T
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1 rrttjiMiinrirnii uuui nfemmf b. F
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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
Page 123 and 124: I I MATERIALS | vunrraoffifiL
Page 125 and 126: SECTION VH MATERIEL SUPPORT IHNAR E
Page 127 and 128: nnsx «**'.w-i -***. TITLE PAGE 7.1
Page 129 and 130: 7- MATERIEL SUPPORT 7.0 IHTflODUCTI
Page 131 and 132: d. Control of repalr-overhaul-modlf
Page 133: ^_ ,(,OlW-i Certain Items, such as
Page 137 and 138: £•.:. • • • •- As --r*;
Page 139 and 140: 8.1 LUHAR LAUNCH COMPLEX The Lunar
Page 141 and 142: environment simultaneously with the
Page 144 and 145: CONFIDENTIAL *"- 'WWW' WDLAR-S-458
Page 146 and 147: »MHBfiimfc I'-V-Iwf^,,,.,.,^... .
Page 148 and 149: CHANGE NO. RECORD OF CHANGES . IESC
Page 150 and 151: «*w **•*-«, •*!:. • • * *
Page 152 and 153: ; £.*. te^Ltj^r&& Personnel *(Spac
Page 154 and 155: '~*3!-.,..,..•-..... ;X*) ^ype IV
Page 156 and 157: ^^s^*f3C^^ L SB6BS .*v^| • e. Qua
Page 158 and 159: ii msr' -fe*fc (2) flight test oper
Page 160 and 161: - "-^m, (2) Training films and tran
Page 162 and 163: I*-? 1 ^ ;: f ,i * Proposed «* Num
Page 164 and 165: ? Major Segment of System Vehicle S
Page 166 and 167: I. ••- ' ttr»*M*w CHABT EC - B
Page 168 and 169: mmjmmmMumammmt sk-.-^^:-/: ^;:-S" :
Page 170 and 171: .; -.
Page 172 and 173: i ssvs-innaM 3 r r • n 99 A3 I V
Page 174 and 175: CY 63 CY 64 CY 65 CY 66 £ i i J F
Page 176 and 177: BT CV 62 CV 63 Ct 6h 23 2S J I A S
Page 178 and 179: ~?t. rW---^=t.-.i?^..-- . .J-: ,> n
Page 180 and 181: jspjiyjziffli^^ ASSESSMENT ASSESSME
Page 182 and 183: 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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