- Page 1 and 2: .. . 92 LUNAR EXPEDITION HEADQUARTE
- Page 3 and 4: GENERAL LUNAR DATA Dlitont* hoiii n
- Page 5 and 6: DOWNGRADED AT 12 YEAR INTERVALS: MO
- Page 7 and 8: ••-a- INDEX + * n3--& TITLE PAG
- Page 9 and 10: CTSf £:* 43 --at an earlier date a
- Page 11 and 12: in 1965.
- Page 13 and 14: 1 FROORAM tamau IB J LUNAR EXPEDITI
- Page 15 and 16: SECTION II PROGRAM BESCRIFTIOH LUHA
- Page 17 and 18: INDEX*- -"-*•••• *r--> •*
- Page 19 and 20: 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 31 and 32: •eWFUBfiH^ At ^s*s* CHANGE NO. £
- Page 33 and 34: 3.0 INTRODUCTION It*** The establis
- Page 35 and 36: » * n * • 3A LUHAR EJCHKDITION T
- Page 37 and 38: ^ ~c tt „£ 9 e i * MASTER PROGRA
- Page 39 and 40: 4 CHART m-8 LUNAR EXPEDITION PROGRA
- Page 41 and 42: e 0- i„* . \ i .* :, %JL ROMAN KN
- Page 43 and 44: - : ! . - . • - . - » • ' ;
- Page 45 and 46: ' >,.. ' » '• • «-• -.•.-
- Page 47 and 48: X X X X X x X X u_ 1L JL fl_ IX IX
- Page 49 and 50: • u - U CY-62 | CY-63 -T* CY-64 -
- Page 51 and 52: -".:-:-$-- -,*ii: "-. i m« iimwiw
- Page 53 and 54: _L X X X X X X X X B_ U- JL B_ M_ U
- Page 55 and 56: SECTION IV lEVELOFMENT - TEST - ERO
- Page 57 and 58: TITLE PAGE RECORD OF CHANGES TSDE3L
- Page 59 and 60: 4. DEVELOFMEHT - 2EST - PRODUCTION
- Page 61 and 62: The Lunar launching Stage must be d
- Page 63 and 64: • : - * * • '•• '^i&.stfl d
- Page 65 and 66: 4.2.1 2 c." 'ControlSystem"***' TJ5
- Page 67 and 68: (£) Tailoring conductivity distrib
- Page 69 and 70: i.^ ffiBF.^-U. 4.2.1.5 .,***• ' H
- Page 71 and 72: &W 5?T" •In B^JJ. . 6950 ( °> --
- Page 73 and 74: 4.2.3.4 > atfti'3 m Shroaghout this
- Page 75 and 76: ii.2-5 GOTDWCE AHD CCmKOL EISTKM fc
- Page 77 and 78: : AHa «* 4.e.5-5 DOPPUK RASAS Anti
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LUKI'lkDflU' ,? 4.2.6 COMPUTER 4.2.
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4.2-7 COMMtflOCATTOBS 4.2.7-1 Die m
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4.2.6.6 NASA intends to measure the
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• •^teiJn*^;^*,* Mlcrotopograpb
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•**• /v.^kiri^ri!21 C(PUO»w> f
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a. Propulsion b. Heat transfer c. A
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4*3-1-1.5 Static Vests—The static
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The Lunar Expedition flight test pr
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d. lunar Landing -and Return The un
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mmmm k.^.k CHECKOUT AMP TEST BJUHMB
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4.U-3 LOCATION It is anticipated th
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-tnautt jaait -BAJKV *&/* c
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RE k-1 JNAR PAZLOAD TOLAR-S^58 T ;
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CSAMGE HO. *e*fff ?*i -iisri'tfSMii
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."W.-»» \ -a • \ ^ V '^liMKK. *
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5-2 COST ESTIMATE^. 5he funding req
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CONFIDENTIAL DIVISION OF LUNAR EXPE
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•;42££*#». - RECCRP OP CHANGES
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£i * - . * • * Intentionally Lef
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h. 5he Flans Office will be respons
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( . , * • : • - . •'--'~--- 6
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7W -V'- mirv PLANS r ^ 1 I LUNAR i
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ATER1ALS l**;* ?* FACILITY DESIGN A
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CHANGE NO. fjAMHffiT''"'" .\','. A
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&f> sfiiHe £•.•* S&- l*J* ,.!.
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mm "Stal^ Determination of quantiti
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: *.--.- minimized • 7 .k REAL PR
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...*:, •*P : -J&3, TITLE PAGE REC
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^^^f -£•'• - j£&a 5*?- SECTIQ
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8. ' CIVIL ENGHJEERIBG 8.0 nnBOKJcn
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-S* *. effected. The use of existin
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e 1E not likely to occur. Skis phil
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T-a^i^^-^-^s:r- l ^Wiir:-v^*i-.-,-M
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• - ' * : . & & a*?'** SECTION IX
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Txnsx v -li. TITLE PAGE • * 9.1 R
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9. PERSQHHEL AND HtAHttJB 9.0 IHBTO
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9.3 PUNNING FACTORS AND GROUND RUI
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2- Lunar lending Stage - Wr.y I965.
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^p'nF -ffiff c ttCDEL .***. «** (b
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w fXSf^wafti^^ magnitude. Provided
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•iSBz* «£ e c. Other Training f
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* Major Segment of System Vehicle S
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Major Segment Cadre of System Requi
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MOOKAM SCMBMM RE-ENTRY VEHICLE CY 6
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- T ^i.. --^-^ =*&- _'• s:Ti:::;y
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c LUNAR LANDING STAGE CY 61 CV 62 C
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Chart DC-El ^ LUNAR LAUNCH STAGE AN
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C J_ J. .1. _Z_ J_ J_ 11. II J2_ JL
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*>*;: •V}-- > »* W 7 ^ e / -+- P
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RE-ENTRY VEHICLE DESIGN EVALUATION
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- -V - " , ' . A~*. iTM|-fr Tmnr"yn
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" :SS=7-
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•J*. - TITIE PAGE. INDEX 10,1 REC
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c c 10. INTELLIGENCE ESTIMATES lo.o
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^*^ Although large orbiting spacecr
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MANNED LUNAR PAYLOAD LUNAR RE-ENTRY
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*• * S K ^ - ^ i S B l * ! - - 1
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•JW"S V. Lunar Expedition Facilit
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Responsive Production Concept A con