LUNAR EXPEDITION PLAN

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&f> sfiiHe £•.•* S&- l*J* ,.!...-."-••• •• Intentionally left Wank. WDIAR-S-1»56 Tkli aKitWftt contain frfamatlW .ffwllnf ft* notlmal aafma at tha Unitoa »M« wllfcto Ma H»Taa at Ik* brXaa* tan. JHW li, U.S.C.. SMIIM W3 owl 7W. Ma ln.inimi ar rmtattan af wkick In ••» Maw to •• «itlM»ri — i- — " M U fc- t—
7- MATERIEL SUPPORT 7.0 IHTflODUCTION It is intended that this program use two significant concepts that will result in better management of the materiel support program. These are the Delayed Procurement Concept and the Responsive Production Concept. Under tiie Delayed Procurement Concept, the ordering and delivery of high-cost insurance-type spares is deferred until the final production run must be made, allowing for the accumulation of maximum operational experience with the new item before a final spares order must be placed. Under the Responsive Production Concept, a portion of the requirement for high-cost operational spares Is procured In unfabricated, unassembled form. When the spares demand can be more reliably predicted, based on actual usage experience, additional complete spare items can be produced within a very short lead-time period. When experience fails to justify a requirement for additional complete spares, the materiels and parts involved can be utilized In end article production. The policy shall be to buy minimum quantities of high-value spares and maintain close control over their transportation, storage, issuance, and repair until they finally wear out, or are no longer required. Simplification of procedures and relaxing of restrictions on low-value items will provide the means (man-power, machine time, etc.) for more precise management of high-value items. 7-1 SUPPLY Maximum utilization will be made of existing assets. Where practical, equipment and parts will be reclaimed from completed test programs, repaired, modified and overhauled to suitable condition for use in later tests and operational tasks. The procedures and paperwork Involved with procurement of spare parts must be streamlined to permit maximum flexibility in planning and responding to a continually changing configuration^ Immediate adjustment or inventories and reorder points must result from test program and engineering changes. Selection of spare parts should be made at the time of initial design to enable procurement of spare and production parts concurrently to eliminate reorder costs resulting from separate procurements. 7-5 -VDLAB-S-l^B Tkli dauMM (antiiai trilatntqlloii oHMtina Ma MllaMl dafMM sf Ih* Unllad JtohH niHiin Hw Menrng •» Hn Ciplonoti lawi. Till* II, U.S.C-, Smalm 793 sad 79a, Hw franmunicn er lavaleUen af which In any mmmr la an •nnrlharlaMl ptrtMi i> erahibiml br 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
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
Page 123 and 124: I I MATERIALS | vunrraoffifiL
Page 125 and 126: SECTION VH MATERIEL SUPPORT IHNAR E
Page 127: nnsx «**'.w-i -***. TITLE PAGE 7.1
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 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
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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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