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    Space Station Propulsion System Technology

    Space Station Propulsion System Technology


    Two propulsion systems have been selected for the space station: O/H rockets for high thrust applications and the multipropellant resistojets for low thrust needs. These thruster systems integrate very well with the fluid systems on the station. Both thrusters will utilize waste fluids as their source of propellant. The O/H rocket will be fueled by electrolyzed water and the resistojets will use stored waste gases from the environmental control system and the various laboratories. This paper presents the results of experimental efforts with O/H and resistojet thrusters to determine their performance and life capability.

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    Titel :

    Space Station Propulsion System Technology

    Beteiligte:
    R. E. Jones (Autor:in) / P. R. Meng (Autor:in) / S. J. Schneider (Autor:in) / J. S. Sovey (Autor:in) / R. R. Tacina (Autor:in)
    Erscheinungsdatum :

    1987

    Format / Umfang :

    18 pages

    Medientyp :

    Report

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Rocket Engines & Motors , Manned Spacecraft , Hydrogen oxygen engines , Resistojet engines , Space stations , Propulsion system configurations , Gases , Hydrolysis , Rocket engines , Thrust , Waste utilization , Waste water

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