A Case Study in NASA-DoD - The Black Vault

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-113- Table A-3 LAUNCH COSTS--NOMINAL CASE ($ millions) Maximum AEM and L-AEM-BL altitude 1000 n mi AEM and L-AEM-BL orientation - Earth only Space shuttle cost/launch - $15.4 million Kick stages - Solid rockets Payloads 114 228 Payloads/spacecraft 13 6 13 6 100% weight attribution AEM/STPSS 37 51 65 93 AEM/MMS 41 63 68 111 STPSS 37 51 60 94 XMS 41 67 65 112 L-AEM 36 50 58 90 AEM/L-AEM 36 50 62 90 L-AEM/MMS 34 51 57 96 AEM/L-AEM/MMS 33 50 57 89 50% weight attribution AEM/STPSS 26 37 48 69 AEM/MMS 27 44 46 77 STPSS MiS 26 28 38 46 42 43 68 77 L-AEM 26 37 42 66 AEM/L-AEM 26 37 46 67 L-AEM/MMS 24 37 39 68 AEM/L-AEM/MMS 24 37 41 66 Service charge AEM/STPSS 16 24 30 44 AEM/MMS 14 24 24 42 STPSS 16 24 25 43 MMS 14 24 22 41 L-AEM 16 24 25 43 AEM/L-AEM 16 24 29 44 L-AEM/MMS 14 24 22 41 AEM/L-AEM/t41S 14 24 24 42 NASA tariff AEM/STPSS 79 127 157 241 AEM/!14S STPSS 83 79 144 126 149 131 258 235 MS 83 146 134 252 L-AEM AEM/L-AEM 85 85 134 133 142 167 247 254 L-AEM/M4S 78 134 129 242 AEM/L-AEM/MMS 77 133 141 242 Modified NASA tariff s AEM/STPSS 35 47 61 87 AE74/HMS 60 90 97 158 STPSS 34 46 55 84 tmS 61 97 92 163 L-AEM 38 51 76 92 AD/L-AEI 44 49 76 99 L-AEM/MMS 42 51 71 92 AEM/L-AEM/MMS. 38 53 66 95 Assumes that whenever possible, the spacecraft and its kick stages will be oriented perpendicular to the shuttle axis.
-114- Table A-4 LAUNCH COSTS FOR UPGRADED AEM ($ millions) Maximum AEM altitude = Geosynchronous AEM orientation - Earth and sun Space shuttle cost/launch = $15.4 million Kick stages = Solid rockets Payloads 114 228 Payloads/spacecraft 13 6 13 6 100% weight attribution AEM/STPSS 34 42 61 81 AEM/MMS 29 43 59 93 50% weight attribution AEM/STPSS 25 33 47 63 AEM/MMS 21 31 43 70 Service charge AEM/STPSS 17 24 32 46 AEM/MMS 12 20 28 44 NASA tariff AEM/STPSS 86 126 168 249 AEM/MMS 65 109 152 259 Modified NASA tariffa AEM/STPSS 39 50 74 95 AEM/MMS 45 64 89 139 aAssumes that whenever possible, the spacecraft and its kick stages will be oriented perpendicular to the shuttle axis.
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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
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 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
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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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