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A Case Study in NASA-DoD - The Black Vault

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-113-<br />

Table A-3<br />

LAUNCH COSTS--NOMINAL CASE<br />

($ millions)<br />

Maximum AEM and L-AEM-BL altitude 1000 n mi<br />

AEM and L-AEM-BL orientation - Earth only<br />

Space shuttle cost/launch<br />

- $15.4 million<br />

Kick stages<br />

- Solid rockets<br />

Payloads 114 228<br />

Payloads/spacecraft 13 6 13 6<br />

100% weight attribution<br />

AEM/STPSS 37 51 65 93<br />

AEM/MMS 41 63 68 111<br />

STPSS 37 51 60 94<br />

XMS 41 67 65 112<br />

L-AEM 36 50 58 90<br />

AEM/L-AEM 36 50 62 90<br />

L-AEM/MMS 34 51 57 96<br />

AEM/L-AEM/MMS 33 50 57 89<br />

50% weight attribution<br />

AEM/STPSS 26 37 48 69<br />

AEM/MMS 27 44 46 77<br />

STPSS<br />

MiS<br />

26<br />

28<br />

38<br />

46<br />

42<br />

43<br />

68<br />

77<br />

L-AEM 26 37 42 66<br />

AEM/L-AEM 26 37 46 67<br />

L-AEM/MMS 24 37 39 68<br />

AEM/L-AEM/MMS 24 37 41 66<br />

Service charge<br />

AEM/STPSS 16 24 30 44<br />

AEM/MMS 14 24 24 42<br />

STPSS 16 24 25 43<br />

MMS 14 24 22 41<br />

L-AEM 16 24 25 43<br />

AEM/L-AEM 16 24 29 44<br />

L-AEM/MMS 14 24 22 41<br />

AEM/L-AEM/t41S 14 24 24 42<br />

<strong>NASA</strong> tariff<br />

AEM/STPSS 79 127 157 241<br />

AEM/!14S<br />

STPSS<br />

83<br />

79<br />

144<br />

126<br />

149<br />

131<br />

258<br />

235<br />

MS 83 146 134 252<br />

L-AEM<br />

AEM/L-AEM<br />

85<br />

85<br />

134<br />

133<br />

142<br />

167<br />

247<br />

254<br />

L-AEM/M4S 78 134 129 242<br />

AEM/L-AEM/MMS 77 133 141 242<br />

Modified <strong>NASA</strong> tariff s<br />

AEM/STPSS 35 47 61 87<br />

AE74/HMS 60 90 97 158<br />

STPSS 34 46 55 84<br />

tmS 61 97 92 163<br />

L-AEM 38 51 76 92<br />

AD/L-AEI 44 49 76 99<br />

L-AEM/MMS 42 51 71 92<br />

AEM/L-AEM/MMS. 38 53 66 95<br />

Assumes that whenever possible, the spacecraft and its<br />

kick stages will be oriented perpendicular to the shuttle<br />

axis.

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