I. 1.4 The MOSES- Concept (TU-Berlin). (MOSES - Modular Solar Energy Satellite) Ground Power Output Total Mass Conversion Efficiency with CR = 2 Total Cost (Without DDT&E) Electricity Cost (1 973 estimate) Module Size Module Power Characteristics:In a low technology advancement scenario the complete modules will be stacked into each other and transported into GEO by a high volume HLLV. In a medium technology advancement scenario only the blankets will be fabricated on Earth. Structure and concentration mirrors will be fabricated in a space factory and then mounted to the blankets. The high technology advancement scenario proposes total space-manufacturing in an automatic facility in space. The modules will be integrated to large solar collectors of variable sizes.
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