LUNAR EXPEDITION PLAN

More documents

Recommendations

Info

li.2 1.3A DYNAMICS ^iia^djajj^fi' (l) Analytical studies In the following areas should be undertaken. speeds. (a) Unsteady aerodynamic forces at hypersonic (b) Aeroelastic changes In structural loading and aerodynamic stability derivatives. 4.2.1.k (c) Flutter (d) Servoelastlc coupling with guidance system. (e) Fatigue due to random loading- (f) Transient dynamic loading. Present projects -within the Air Force applied research program will be reviewed and reoriented or effort increased, as appropriate, to provide the necessary data. Projects which can be used for this purpose are listed below; 6lT3*(U) Study of Controlled Final Deceleration Stages for Recoverable Vehicles. 1315 (U) Bearings and Mechanical Control Systems for Flight Vehicles. 1366 (U) Construction Techniques and Applications of Mew >feterials. 1370 (U) Dynamic Problems in Flight Vehicles. 1395 (U) Flight Vehicle Design. 6lU6 (U) Flight Vehicle Environmental Control. 1309 (U) Flight Vehicle Environmental Investigation. 6065 (u) Performance and Designed Deployable Aerodynamic Decelerations 4.13 WJ1IAB-S-45S Tall docaaian) oaioini inlonnatlgn affactint Ilia nulloiwl dafau* ef ttia Unita4 Vp
i.^ ffiBF.^-U. 4.2.1.5 .,***• ' H v. In addition to the applied research efforts referred to in Paragraph 4.2.1.1* an intensive study of re-entry vehicle characteristics required for the tunex mission is being accomplished under project 7990 task 17532- 2fcis study will define an optimum vehicle configuration and present the most feasible technical approaches to solving the various re-entry problems. For example, the desirability of ablative and/or radiation techniques for cooling will be determined. h.lk WDLAR-S-456 •yO, . ./***S» TMt dMV»aM IMtoliM tahVBMlafl affMtfrti
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 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 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 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 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 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
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 • . , ;
show all

LUNAR EXPEDITION PLAN

Create successful ePaper yourself

Delete template?

Save as template?