LUNAR EXPEDITION PLAN

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.. . 92 LUNAR EXPEDITION HEADQUARTE
Page 3 and 4:
GENERAL LUNAR DATA Dlitont* hoiii n
Page 5 and 6:
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
Page 15 and 16:
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
Page 38 and 39:
• k- . *-, ^ CY IS CY* C Vi'ONDJF
Page 40 and 41:
pf 4 _-$» AL
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PKMIAM KHNU - 6 Years **»?. m D LU
Page 44 and 45:
MOOtAM SCHBUU - 6 Years TTT TJ (Con
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'**%' 8S*-S-HV r ia.W.
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i i-fli'- IHJI.I- 1 n fi "3a. as^-s
Page 50 and 51:
- 6 Years IIT-F j LUNEX CIVIL ENGIN
Page 52 and 53:
CY-66 CY -67 CY-6C JFfllNJJlSONDJFM
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ssf-s-svnaA .1 _ ijH ,-, w-« £9-A
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CHANGE NO. T .RECORD OP CHANGES INS
Page 58 and 59:
**i*$& 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 îia^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
Page 74 and 75:
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
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•** tWKfltWTlAIr In order to dete
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A^wt; 4.2.9 MATERIALS ^!C» w 4.2-9
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k-3 TEST PLAN
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«**& 2heee tests vill provide data
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«,..*.» vMln *• mmlng of iha fi
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difficult step. Jhe major testing s
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a. Evaluate the effects of engine b
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k.h mODJCTim PLAff **i '**^4 At the
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I. . FKOHE 4-3 ' i GENERAL ARRANGEM
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"7 *"4C'" "-?•• FIGURE lf-1 MAH
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S3CTIC5I V BODGST /JH) FIHAI7CIAL L
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INBEX ***•••*: ;2* TITLE PAGE
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**!-
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5-3 FY 62, 63 FINANCIAL PLAN MANNED
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EECTIOH VI PROGRAM MANAGEMENT LUNAR
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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 and 134: ^_ ,(,OlW-i Certain Items, such as
Page 135 and 136: d. Altitude Simulation Unit - - A p
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 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
Page 184 and 185: CHANGE NO. i t. RECORD OP CHANGSS D
Page 186 and 187: Site 1 - •T'Z • This page inten
Page 188 and 189: pound thrust. The estimated tine fo
Page 190 and 191: V Actual accomplishment of the proj
Page 192 and 193: c MANNED 'LUNAR PAYLOAD cam LUNAR R
Page 194 and 195: ; - = * f t - •*TTF «... s.'. \
Page 196 and 197: __?_. ***** (JUBMFU u.'i -* __ ^ ^
Page 198: tf *SS- TTAT Lunar Chart • . , ;
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LUNAR EXPEDITION PLAN

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