Central static invertor used to establish 1250-va, 115/200-v, three-phase 400-cps AC power distribution for Apollo Spacecraft Command and Service Module


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    Title :

    The central inverter in a spacecraft power system.


    Contributors:
    Bowles, D. L. (author) / Geyer, M. A. (author) / Kernick, A. (author)


    Publication date :

    1966-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    The Central Inverter in a Spacecraft Power System

    Bowles, David L. / Geyer, Manvel A. / Kernick, Andress | IEEE | 1966



    Central-station electric power for spacecraft

    Grey, J. / Deschamps, L. | Tema Archive | 1989


    Design of a Thermally-Integrated 200- kW Spacecraft Power Inverter

    GIELLIS, R. / CULLIMORE, B. / PISTOLE, R. | AIAA | 1984


    Development of a rotary power transformer and inverter drive for Spacecraft

    McLyman, C.W. / Bridgeforth, A.O. | Tema Archive | 1983