The power requirement of vehciles desgined to transport cargo supporting a piloted expedition to Mars is in the range of megawatts. Therefore, it is imperative that the megawatt - class power processing unit designed for high-power nuclear electric propulsion vehicles using turboalternators and advanced magnetoplasmadynamic thrusters shouls be such that the overall system efficienty is as high as possible with minimum system specific mass.


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    Titel :

    Evaluation of Cryogenic Power Conditioning Subsystems for Electric Propulsion Spacecraft


    Beteiligte:
    Frisbee, R. (Autor:in) / Krauthamer, S. (Autor:in) / Das, R. (Autor:in)

    Erscheinungsdatum :

    11.08.1996


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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