A Case Study in NASA-DoD - The Black Vault

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FIGURES
1. STP Standard Spacecraft ................................... 38
2. Modular Multimission Spacecraft ........................... 40
3. Applications Explorer Spacecraft .......................... 42
4. L-AEM Configuration ........................................ 43
5. Baseline Space Test Program Orbit Options ................. 55
6. Spacecraft Unit Cost Versus Weight ........................ 59
7. Effect of the Maximum Number of Payloads per Spacecraft
(nominal case) ........................................ 68
8. All-STPSS Nominal Case ..................................... 70
9. Effect of Space Test Program Size (nominal case) .......... 71
10. Distribution of Program Costs (L-AEM Option) . ........... 81
B-1. Power and Distribution Subsystem Block Diagram ............ 120
B-2. STPSS Power Subsystem ....................................... 123
B-3. MMS Block Diagram--Power Subsystem Module ................. 124