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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-81-<br />
COST<br />
LAUNCH COSTS<br />
(Millions of<br />
Dollars M US PRORATED<br />
250 - <strong>NASA</strong> TARIFF<br />
200 - MODIFIED <strong>NASA</strong> TARIFF<br />
NOMINAL CASE:<br />
114 PAYLOADS<br />
6 MAX. PISC<br />
50<br />
N h<br />
SPACECRAFT $15.4 Million S30 Million $15.4 Million $30 Million<br />
SHUTTLE SHUTTLE, SHUTTLE S UTTLE<br />
WESTERN TEST RMGE LAUNCH EASTERN TEST RANGE LAUNCH<br />
COSTS<br />
COSTS<br />
Fig. 10-Distribution of program costs<br />
(L-AEM option)<br />
exceed $100 million. <strong>The</strong> most significant factor is the orbit <strong>in</strong>cl<strong>in</strong>ation.<br />
<strong>The</strong> use of the modified <strong>NASA</strong> tariff rate redresses this drastic<br />
cost imbalance. <strong>The</strong> variation <strong>in</strong> shuttle cost considered <strong>in</strong> this study<br />
does not appear to greatly alter the launch costs, provid<strong>in</strong>g the earlier<br />
<strong>NASA</strong> tariff rate is not used.<br />
jt<br />
CONCLUSIONS<br />
Four major conclusions have been drawn from this case study. First,<br />
progrma coat does not proiide a basis for choos<strong>in</strong>g amng the ARM, STPSS,<br />
adMS spacecraft, given their present designs. Only when the modified<br />
<strong>NASA</strong> tariff schedule was used for allocat<strong>in</strong>g the shuttle launch cost did<br />
the STPSS options become preferred; with the uncerta<strong>in</strong>ty <strong>in</strong> the appropriateness<br />
of this tariff schedule, this case does not provide sufficient basis<br />
for recommend<strong>in</strong>g the STPSS development.<br />
Second, the avaiZability of the L-AE1. spacecraft, or some vezr similtar<br />
design, would provide a basis for m<strong>in</strong>imiz<strong>in</strong>g the co t of the Air Force's<br />
Space Test Program. <strong>The</strong> L-AEM could be used <strong>in</strong>dividually or <strong>in</strong> comb<strong>in</strong>ation<br />
with the AE1 and/or MI(S as the missions require. <strong>The</strong> upgraded AEM<br />
options, although hav<strong>in</strong>g program costs similar to the L-AEM options,<br />
provide less capability for handl<strong>in</strong>g growth <strong>in</strong> the Space Test Program<br />
mission model.