14-10a Mission 6 - Subassembly Build-up 14-17 14-10b Mission 5A - Test Matrix 14-17 14-Ila Mission 7 - Rotary Joint Assembly 14-18 14-llb Mission 7 - Test Matrix 14-18 14-12a Mission 8 - Antenna to Rotary Joint Interface 14-20 14-12b Mission 8 - Test Matrix 14-20 14-13a Mission 9 - Central Mast Assembly and Integration Test 14-21 14-13b Mission 9 - Test Matrix (Conducting Mast Assembly) 14-21 14-14 Mission 11 - Test Matrix 14-24 14-15 OTF Antenna 14-24 14-16 OTF Power Densities 14-25 14-17 MPTS Orbital Test Program ROM Costs 14-27 14-18 Critical Technology Schedule 14-29 14-19 MPTS Orbital Test Program ROM Cost Summary 14-29 J-1 Total Cost Summary Format J-2 J-2 Total Cost Summary - Initial Operational Systems With Minimum A^ J-4 J-3 Total Cost Summary - Operational System (Goal) J-11 J-4 Total Cost Summary - Initial Operational System Using At = 64. 7 x 104 m2 J-22 J-5 Summary of Initial and Final Operational System Characteristics J-29 J-6 Capital Cost to Energy Cost Conversion Versus Rate of Return J-30 J-7 SPS Capital Cost/Transportation Cost for Various Power Source Characteristics J-31 J-8 SPS Energy Cost/Transportation Cost for Various Power Source Characteristics J-32 J-9 SPS Energy Cost/Transportation Cost for Various Rates of Return J-33 J-10 SPS Energy Cost/Transportation Cost for Various Construction Cycles J-34 K-1 Summary of Ground Test Objectives/Implementation K-2 K-2 Ionospheric Effects K-4
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