A concise but complete system description for the preferred concept of the Solar Power Satellite System is presented. Significant selection decisions included the following: (1) single crystal silicon solar cells; (2) glass encapsulated solar cell balnkets; (3) concentration ratio 1; (4) graphite composite materials for primary structure; (5) electric propulsion for attitude control; (6) klystron RF amplifier tubes for the transmitter; (7) one kilometer diameter transmitter with a design transmission link output power of 5,000 megawatts; (8) construction in low earth orbit with self-powered transfer of satellite modules to geosynchronous orbit; and (9) two-stage winged fully reusable rocket vehicle for transportation to low earth orbit.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Solar Power Satellite System Definition Study. Part 3: Preferred Concept System Definition


    Publication date :

    1978


    Size :

    364 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English