A Case Study in NASA-DoD - The Black Vault
A Case Study in NASA-DoD - The Black Vault
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.