A Case Study in NASA-DoD - The Black Vault

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-109- Table A-1 SPACECRAFT COSTS--NOMINAL CASE ($ millions) Maximum AEM and L-AEM-BL altitude = 1000 n mi AEM and L-AEM-BL orientation - Earth only Payloads 114 228 Payloads/spacecraft 13 r 6 13 1I 6 Spacecraft Type Cost AEM 2.3 6.8 11.4 16.0 STPSS Nonrecurring 22.9 22.9 26.9 26.9 Spin .... 26.2 40.5 Low-cost 57.1 90.7 67.8 110.9 Precision 35.0 34.3 41.8 47.5 Total 117 155 174 242 AEM 2.3 9.1 11.4 20.5 MKS 108.8 162.5 155.6 251.1 Total 111 172 167 272 STPSS Nonrecurring 22.9 22.9 26.9 26.9 Spin .... 20.0 41.6 Low-cost 62.5 109.6 88.4 150.1 Precision 34.5 34.2 43.6 52.1 Total 120 167 179 271 MKS 117 190 176 297 L-AEM Nonrecurring 9.8 9.8 11.3 11.3 Spin .... 14.3 31.1 Precision 86.9 123.9 108.9 168.3 Total 97 134 135 211 L-AEM Nonrecurring 11.9 11.9 14.5 14.5 Baseline 20.4 29.6 19.0 31.4 Spin .... 15.2 32.4 Precision 29.5 28.7 33.1 36.5 STPSS Nonrecurring 18.4 18.4 18.4 18.4 Low-cost 41.5 73 63.5 106.2 Total 122 162 164 239
-110- Table A-I (Cont.) Payloads 114 228 Payloads/spacecraft 13 6 137 6 Spacecraft Type Cost L-AEM Nonrecurring 11.9 11.9 14.5 14.5 Baseline 18.7 26.8 17.9 29.8 Spin -- -- 14.3 31.0 Precision 65.1 93.4 88.2 133.7 Total 96 132 135 209 AEM 2.3 6.9 11.4 16.0 L-AEM Nonrecurring 11.9 11.9 14.5 14.5 Baseline 14.2 13.6 4.5 4.3 Spin -- -- 21.5 31.3 Precision 65.8 94.4 88.8 135.3 Total 94 127 141 201 L-AEM Nonrecurring 9.8 11.9 11.3 11.3 Baseline -- 26.8 -- -- Spin -- -- 3.8 10.8 Precision 58.5 93.4 76.6 104.1 MMS 33.7 -- 58.5 142.5 Total 102 132 150 269 AEM 2.3 9.1 11.4 20.5 L-AEM Nonrecurring 9.8 9.8 11.3 11.3 Spin -- -- 3.8 10.8 Precision 58.5 96.2 76.6 104.1 MMS 25.5 16.5 34.3 80.4 Total 96 132 137 227
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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
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 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
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-159- Appendix H PROGRAM OPTIONS FO
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I 4 I IQ. w ~ w 01 " 1 I I I I 0 .c
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-163- Table H-4 ORBIT 2: PAYLOAD AS
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-165- c0 k- c" Q N 3- W 0 0 IT -- c
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-167- Table 1-7 CASE I (A)a PROGRAM
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-169- Table H-9 CASES I (K) AND V (
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-171- Table H-11 CASE II(B) PROGRAM
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-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
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-181- Table Hi-21 CASE V (E) PROGRA
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-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
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