A spacecraft propulsion system comprises two thrusters, each operating in accordance to a corresponding propulsion technique. A controller is configured to direct collected solar energy to heat a propellant for consumption in one of the two thrusters, or to generate electric energy for the other one of the two thrusters.


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    Title :

    Space Mission Energy Management Architecture


    Contributors:

    Publication date :

    2021-07-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Space mission energy management architecture

    SERCEL JOEL / MITCHELL AARON | European Patent Office | 2022

    Free access

    Space Mission Energy Management Architecture

    SERCEL JOEL / MITCHELL AARON | European Patent Office | 2022

    Free access



    A Multi-Mission Space Avionics Architecture

    Chau, S. N. / Reh, K. R. / Cox, B. et al. | British Library Conference Proceedings | 1996