The results of testing a high voltage electrical power system (EPS) breadboard using high voltage power processing equipment developed at Marshall Space Flight Center and Ni-Cd batteries are discussed. These test results are used to extrapolate to an efficient, reliable, high capacity EPS for near term low Earth orbit, high power applications. EPS efficiencies, figures of merit, and battery reliability with a battery protection and reconditioning circuit are presented.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    High Voltage Electrical Power System for Low Earth Orbit Applications


    Contributors:
    J. R. Lanier (author) / J. R. Bush (author)

    Publication date :

    1984


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English