A two phase program was conducted to define requirements and to prepare a preliminary design of a test motor system that will accurately and economically simulate the chamber environments of present and future large solid propellant rocket motors. A segmented motor configuration with 28-in. outside diameter case bonded propellant grains was selected. The nominal grain configuration is an internal burning cylinder with both ends burning.


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    Title :

    Ballistic Missile Propellant Evaluation Test Motor System (Super BATES)


    Contributors:

    Publication date :

    1974


    Size :

    219 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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