LUNAR EXPEDITION PLAN

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50899 (u) Molecular Amplification Techniques W27 (u) Self-Contained Electromagnetic Techniques for Space Navigation 4431 (U) Inertial System Components H169-II (U) Space Adapted Celestial bracking System W169-III (U) Jttltl -Headed Solid State Celestial Tracker WI69-IV (U) Solid State Celestial Body Sensors 5201 (u) Inertial Systems Technique 5215 (U) Military Lunar Vehicle Guidance 50320 (U) Military Lunar Vehicle Guidance Systems 58321 (U) Military lunar Vehicle Terminal Guidance •—mm-** WDLAR-S-458 Tktf oaciiaWtt caalaini biletrtatlaq altoclInB fb* Mtiaftot dMania af Mia United Stataa within |ha naanlna af the Eipioinoa tan, THIa II, U.S.C., SMiaa 7*3 and 794, MM hammiulan or nvfloiwn of which in on* noiinw tar *n unsutharlud aadan ii prohibited fay to*.
LUKI'lkDflU' ,? 4.2.6 COMPUTER 4.2.6.1 The United states has the ability to provide a suitable computer facility at the present tine to support the LUNEX mission. As the milestones in the program are realized and requirements become more complex, the computer capability will improve to meet the Be more stringent requirements. Detailed studies on the specific needs of the missions, time-phased, will be conducted to determine trade-offs among possible techniques to insure that machine sophistication does not become an end unto itself. 3be following guidelines providing adequate flexibility, have been followed in arriving at -the required development recommendations: a. Manned vehicles will require extensive data reduction to give an operator real-time display of the conditions around him and solutions to problems such as, velocity and attitude corrections, etc. b. Sensor control (aiming and sampling rate} and data processing will be accomplished on the vehicle either on ground command, or by operator direction. c. Kid-course and terminal guidance requirements will make severe demands upon vehicle-borne computational systems. d. Badlatlon hazards and effects which are unknown at present could influence the technology that will be utilised for lunar missions. e. Emergency procedures must be available in the event that the operators become incapacitated and Incapable of returning to earth at any time during the mission. 4.2.6.2 me Computer Capability can be expanded in two basic ways by improved hardware, or nev concepts. Examples of nev approaches which will be reviewed prior to selection of the final vehicle design are the following: a. Standardized computer functions incorporated into modules so that they can be used to "build" the capability each mission requires. Such e concept would allow a vehicle designer to fabricate a coatputational^facllity without resorting to extensive redesign and/or re-packaging. The modularized concept noted above Is particularly adapted to unmanned missions. 4.24 WDIAB-S-458 .*nci w* Thti •Oiinaiit uMdiu kifwmotian oKaHllig Hit notlml aWaMa of riw United Slata wjttln ttw naanina *f Ik* Ewlwma* 1M, THta tl, U.S.C., SKI1«H 7*3 mvl 794, la* haumliilaii or rvnloflaa •* vnifli In any a w to an •naHltwina' •*[«• h rrahlMM by law. • •/
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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
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 72 and 73: 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
Page 76 and 77: will be attainable. Also, no diffic
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 and 128: nnsx «**'.w-i -***. TITLE PAGE 7.1
Page 129 and 130:
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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