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LEYEL r o R-2619-RC May 1980 Standa
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SECUNITY CLASSIFICATION OF Twa PAGE
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Standard 5pacecraft.ProcurementL_ A
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-ivas representing the official vie
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the missions required. Third, the p
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ACKNOWLEDGMENTS I gratefully acknow
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-xii- VI. APPLYING THE NASA-DOD COO
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-. - am~rumn -xv- TABLES 1. Nominal
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-Xvii- 11-19. Case IV(N)...........
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-xx- L-ANX - Large Diameter Applica
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-1- I. INTRODUCTION The National Ae
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-3- development. Finally, the polic
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-5- of which spacecraft would enabl
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-7- II. U.S. SPACE PROGRAM: DEVELOP
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-9- thought. (8 ) The launching of
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-1- had shown great alarm or acknow
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-13- for other purposes. ,(15) it w
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-15- and that determination as to w
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-17- program and the coordination o
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t -19- legislation, messages, petit
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-21- of the continuing Soviet accom
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-23- Subsequently, the Director of
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-25- to be asked by one of the agen
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-27- space systems; operational sys
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-29- no near-earth orbit manned ope
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ImP, ~ ~ ~~~~ ......... ~~~~~~~~~~~
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-33- 5. Using off-the-shelf, space-
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-35- 1. Spacecraft configurations a
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-37- STANDARD SPACECRAFT DESCRIPTIO
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-39- The payload cluster, while uni
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-41- payload or propulsion, is abou
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-43- z z 0 0 - 0r CL 0 E 4 41- u- 0
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-45- The STPSS can carry a nominal
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i -47- orbit-adjust module, while t
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-49- M9IS The basic MMS, summarized
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-51- 1980-1990 time period are divi
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-53- about 7.5 payloads per spacecr
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-55- 0- - - - - - - - - - cc - - -
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-57- STPSS (STPSS-LC) spacecraft ca
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-59- Table 7 ESTIMATED UNIT 1 COST
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-61- Nonrecurring Costs. Nonrecurri
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-63- where SRU = Service Rendered U
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-65- IV. STANDARD SPACECRAFT ACQUIS
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-67- The costs associated with thes
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-69- to increase to 13. That was fo
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-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 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
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-175- Table H-15 CASE 111(M) PROGRA
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-177- Table H-17 CASE IV(D) PROGRAM
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-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
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-185- Appendix J AIR FORCE AND NASA
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MEMORANDUM OF AGRE1MENT ON THE PROC
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-189- 2.2 DOD SPACE TEST PROGRAM: T
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-191- l4.1.7 STP will review the HF
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I -193- 5.0 NASA AND DOD FINANCIAL
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-195- 5.4.3 Post Delivery Phase: NA
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I '-197- $4 .0 0 A 0 f-4 ;C:ur 0 V
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t 4 In I Io H 0p Ad ~t m 00 -199- E
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-201- COPIED August 24, 1976 Honora
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-204- 13. "The National Space Progr
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-206- 39. Tec hnical vpoaal for a M