The equipment, exclusive of thrustors, required to demonstrate the feasibility of a resistojet propulsion system for space station attitude control application using representative simulated crew biowaste propellants and available resistojet thrustors in the ground simulation tests is discussed. The overall objective of the program was to provide a biowaste resistojet prototype propellant management and control system sufficiently similar to the flight article to permit concept feasibility and system demonstration testing of interface compatibility, operational characteristics, and system flexibility.


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    Title :

    Development of a biowaste resistojet propulsion system


    Publication date :

    1973-07-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Development of a biowaste resistojet

    Halbach, C. R. / Yoshida, R. Y. | NTRS | 1971


    Development of a biowaste resistojet

    Halbach, C. R. / Yoshida, R. Y. | NTRS | 1970


    Development of a biowaste resistojet

    HALBACH, C. / YOSHIDA, R. | AIAA | 1970


    Development of a biowaste resistojet

    HALBACH, C. R. / YOSHIDA, R. Y. | AIAA | 1971