Figure VII-1.- SPS mission scenario. Concept 2: The "TRUSS" SPS configuration constructed and assembled primarily in GEO. Chemical COTV transportation from LEO to GEO. Concept 3: The "TRUSS" SPS configuration constructed and partially assembled in LEO with final assembly in GEO. Self-powered transportation from LEO to GEO. Program models have been developed for each of the preceding concepts to identify the following program requirements for each year. 1. SPS units constructed 2. Total SPS units on line 3. Mass to GEO and LEO 4. Operational base units implemented and total on line 5. Personnel in GEO and LEO for production and maintenance 6. New POTV, COTV, PLV, and HLLV units required 7. Personnel and cargo launch vehicle total flights and flight rate to LEO 8. Personnel and cargo orbital transfer vehicle total flight and flight rate to GEO 9. Personnel and cargo launch and orbital transfer vehicles fleet size
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