• No space transportation costs for solar array materials; '/io transportation costs for antenna components • Three 20 km diameter Earth rectenna stations • Steerable rectenna elements receive power up to 60° off zenith • Information management, communications, and program management costs twice 1977 reference SPS (2 separate lunar power stations) • No lunar base costs included A detailed cost comparison is given in Table 1. TABLE 1 COST COMPARISON STATEMENT FOR GEOSYNCHRONOUS SPS AND LUNAR-BASED POWER
RkJQdWJsaXNoZXIy MTU5NjU0Mg==