This paper provides a survey of hydogen/oxygen (H/O) auxiliary propulsion system (APS) concepts and low thrust H/O rocket technology. A review of H/O APS studies performed for the Space Shuttle, Space Tug, Space Station Freedom, and Advanced Manned Launch System programs is given. The survey also includes a review of low thrust H/O rocket technology programs, covering liquid H/O and gaseous H/O thrusters, ranging from 6600 N to 440 mN thrust. Ignition concepts for H/O thrusters and high-temperature, oxidation-resistant chamber materials are also reviewed.


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    Title :

    Hydrogen/oxygen auxiliary propulsion technology


    Contributors:

    Publication date :

    1991-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Hydrogen/Oxygen Auxiliary Propulsion Technology

    B. D. Reed / S. J. Schneider | NTIS | 1991


    Hydrogen/oxygen auxiliary propulsion technology

    REED, BRIAN / SCHNEIDER, STEVEN | AIAA | 1991


    Hydrogen/oxygen auxiliary propulsion technology

    Reed, Brian D. / Schneider, Steven J. | NTRS | 1991