A Case Study in NASA-DoD - The Black Vault

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-xx- L-ANX - Large Diameter Applications Explorer Mission L-AEM-BL - Baseline Configuration of L-AEM L-AEM-P - Precision Configuration of L-AEM L-AEM-S - Spinning Configuration of L-AEM LHCP - Left-Hand Circular Polarization MNS - Multimission Modular Spacecraft MOA - Memorandum of Agreement MODS - Manned Orbital Development System MOL - Manned Orbiting Laboratory N2H 4 - Hydrazine NACA - National Advisory Committee for Aeronautics NASA - National Aeronautics and Space Administration NASC - National Aeronautics and Space Council NiCd - Nickel Cadmium PCM - Pulse Code Modulation PMP - Premodulation Processor PROM - Programmable Read Only Memory PRU - Power Regulation Unit PSK - Phase-Shift Keying RCS - Reaction Control System RFP - Request for Proposal RHCP - Right-Hand Circular Polarization SAGE - Stratospheric Aerosol Gaseous Experiment SAMSO - Space and Missile Systems Organization SGLS - Space Ground Link System SIRE - Solar Infrared Experiment S14H - Solar Maximum Mission SMS - Small Multimission Modular Spacecraft SPS - Space Propulsion System SRU - Service Rendered Units STACC - Standard Telemetry and Command Components STDN - Space Tracking and Data Acquisition Network STP - Space Test Program STPSS - Space Test Program Standard Satellite STPSS-LC - Low Cost Configuration of STPSS ... _
-xxi- STPSS-P - Precision Configuration of STPSS STPSS-S - Spinning Configuration of STPSS STS - Space Transportation System TBD - To Be Determined TDRSS - Tracking and Data Relay Satellite System TRW - Thompson Rino Woolridge VHF - Very High Frequency WTR - Western Test Range
Page 2 and 3: LEYEL r o R-2619-RC May 1980 Standa
Page 4 and 5: SECUNITY CLASSIFICATION OF Twa PAGE
Page 6 and 7: Standard 5pacecraft.ProcurementL_ A
Page 8 and 9: -ivas representing the official vie
Page 10 and 11: the missions required. Third, the p
Page 12 and 13: ACKNOWLEDGMENTS I gratefully acknow
Page 14 and 15: -xii- VI. APPLYING THE NASA-DOD COO
Page 16 and 17: -. - am~rumn -xv- TABLES 1. Nominal
Page 18 and 19: -Xvii- 11-19. Case IV(N)...........
Page 22 and 23: -1- I. INTRODUCTION The National Ae
Page 24 and 25: -3- development. Finally, the polic
Page 26 and 27: -5- of which spacecraft would enabl
Page 28 and 29: -7- II. U.S. SPACE PROGRAM: DEVELOP
Page 30 and 31: -9- thought. (8 ) The launching of
Page 32 and 33: -1- had shown great alarm or acknow
Page 34 and 35: -13- for other purposes. ,(15) it w
Page 36 and 37: -15- and that determination as to w
Page 38 and 39: -17- program and the coordination o
Page 40 and 41: t -19- legislation, messages, petit
Page 42 and 43: -21- of the continuing Soviet accom
Page 44 and 45: -23- Subsequently, the Director of
Page 46 and 47: -25- to be asked by one of the agen
Page 48 and 49: -27- space systems; operational sys
Page 50 and 51: -29- no near-earth orbit manned ope
Page 52 and 53: ImP, ~ ~ ~~~~ ......... ~~~~~~~~~~~
Page 54 and 55: -33- 5. Using off-the-shelf, space-
Page 56 and 57: -35- 1. Spacecraft configurations a
Page 58 and 59: -37- STANDARD SPACECRAFT DESCRIPTIO
Page 60 and 61: -39- The payload cluster, while uni
Page 62 and 63: -41- payload or propulsion, is abou
Page 64 and 65: -43- z z 0 0 - 0r CL 0 E 4 41- u- 0
Page 66 and 67: -45- The STPSS can carry a nominal
Page 68 and 69: i -47- orbit-adjust module, while t
Page 70 and 71:
-49- M9IS The basic MMS, summarized
Page 72 and 73:
-51- 1980-1990 time period are divi
Page 74 and 75:
-53- about 7.5 payloads per spacecr
Page 76 and 77:
-55- 0- - - - - - - - - - cc - - -
Page 78 and 79:
-57- STPSS (STPSS-LC) spacecraft ca
Page 80 and 81:
-59- Table 7 ESTIMATED UNIT 1 COST
Page 82 and 83:
-61- Nonrecurring Costs. Nonrecurri
Page 84 and 85:
-63- where SRU = Service Rendered U
Page 86 and 87:
-65- IV. STANDARD SPACECRAFT ACQUIS
Page 88 and 89:
-67- The costs associated with thes
Page 90 and 91:
-69- to increase to 13. That was fo
Page 92 and 93:
-71- 500 * STPSS 400 AW-STPSS PROGR
Page 94 and 95:
-73- The implications of the forego
Page 96 and 97:
-75- option. Other candidates becom
Page 98 and 99:
-77- the Air Force's Space Test Pro
Page 100 and 101:
-79- decrease any total program cos
Page 102 and 103:
-81- COST LAUNCH COSTS (Millions of
Page 104 and 105:
-83- V. NASA-DOD COOPERATION: ORGAN
Page 106 and 107:
-85- the MHS program stemmed from t
Page 108 and 109:
-87- The Air Force had studied the
Page 110 and 111:
-89- Air Force Headquarters to NASA
Page 112 and 113:
-91- turns out, NASA had agreed to
Page 114 and 115:
also evaluate whether or not adequa
Page 116 and 117:
-95- design, mission model, cost es
Page 118 and 119:
-97- Force interface was retained,
Page 120 and 121:
-99- experience and by identifying
Page 122 and 123:
. . . . . . . -.. . . . . . . . . .
Page 124 and 125:
-103- the nation and other governme
Page 126 and 127:
-105- Appendix A ESTIMATES OF COST
Page 128 and 129:
-107- RANGE OF BIDS Item Range ($ t
Page 130 and 131:
-109- Table A-1 SPACECRAFT COSTS--N
Page 132 and 133:
'I FI Table A-2 SPACECRAFT COSTS WI
Page 134 and 135:
-113- Table A-3 LAUNCH COSTS--NOMIN
Page 136 and 137:
-115- Table A-5 LAUNCH COSTS FOR TH
Page 138 and 139:
Table B-I POWER SYSTEM COMPARISONS
Page 140 and 141:
-119- NOTES TO TABLE B-I (Cont.) mo
Page 142 and 143:
-121- The duration of the data pass
Page 144 and 145:
-123- INNNU AWA n -. s vo (I T 'API
Page 146 and 147:
-125- each battery has its own char
Page 148 and 149:
-127- Table B-2 POWER SUMMARY Chara
Page 150 and 151:
-129- Appendix C COMMUNICATIONS AND
Page 152 and 153:
-131- chiefly for storing commands
Page 154 and 155:
-133- Table C-2 C&DH CHANGES REQUIR
Page 156 and 157:
-135- Table C-3 C&DH CHANGES REQUIR
Page 158 and 159:
-137- NOTES TO TABLE C-3 (Cont.) we
Page 160 and 161:
- 139- Table D-1 ATTITUDE CONTROL A
Page 162 and 163:
* -141- and three reaction wheels a
Page 164 and 165:
-143- by the commonly adopted desig
Page 166 and 167:
-145- Table E-l--Continued I Unit T
Page 168 and 169:
-147- flight-proven elastomeric dia
Page 170 and 171:
-149- Appendix F STRUCTURAL SUBSYST
Page 172 and 173:
-151- points are provided by three
Page 174 and 175:
-153- Table F-2 STPSS STRUCTURAL CO
Page 176 and 177:
-155- Appendix G THERMAL CONTROL SU
Page 178 and 179:
-157- sunlight. These surfaces incl
Page 180 and 181:
-159- Appendix H PROGRAM OPTIONS FO
Page 182 and 183:
I 4 I IQ. w ~ w 01 " 1 I I I I 0 .c
Page 184 and 185:
-163- Table H-4 ORBIT 2: PAYLOAD AS
Page 186 and 187:
-165- c0 k- c" Q N 3- W 0 0 IT -- c
Page 188 and 189:
-167- Table 1-7 CASE I (A)a PROGRAM
Page 190 and 191:
-169- Table H-9 CASES I (K) AND V (
Page 192 and 193:
-171- Table H-11 CASE II(B) PROGRAM
Page 194 and 195:
-173- Table H-13 CASE 111(C) PROGRA
Page 196 and 197:
-175- Table H-15 CASE 111(M) PROGRA
Page 198 and 199:
-177- Table H-17 CASE IV(D) PROGRAM
Page 200 and 201:
-17 9- Table H-19 CASE IV(N) PROGRA
Page 202 and 203:
-181- Table Hi-21 CASE V (E) PROGRA
Page 204 and 205:
-183- Table H-23 CASE VI(F) PROGRAM
Page 206 and 207:
-185- Appendix J AIR FORCE AND NASA
Page 208 and 209:
MEMORANDUM OF AGRE1MENT ON THE PROC
Page 210 and 211:
-189- 2.2 DOD SPACE TEST PROGRAM: T
Page 212 and 213:
-191- l4.1.7 STP will review the HF
Page 214 and 215:
I -193- 5.0 NASA AND DOD FINANCIAL
Page 216 and 217:
-195- 5.4.3 Post Delivery Phase: NA
Page 218 and 219:
I '-197- $4 .0 0 A 0 f-4 ;C:ur 0 V
Page 220 and 221:
t 4 In I Io H 0p Ad ~t m 00 -199- E
Page 222 and 223:
-201- COPIED August 24, 1976 Honora
Page 224 and 225:
-204- 13. "The National Space Progr
Page 226 and 227:
-206- 39. Tec hnical vpoaal for a M
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