This is a presentation of view graphs. The design parameters are given for the redesigned solid rocket motor (RSRM), the Advanced Solid Rocket Motor (ASRM), Space Shuttle Main Engine (SSME), Solid Rocket Booster (SRB) separation motor, Orbit Maneuvering System (OMS), and the Reaction Control System (RCS) primary and Vernier thrusters. Space shuttle propulsion issues are outlined along with ASA program definition, ASA program selection methodology, its priorities, candidates, and categories.


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    Title :

    Space shuttle propulsion systems


    Contributors:


    Publication date :

    1991-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Space Shuttle Propulsion Systems

    R. Bardos | NTIS | 1991





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