Computer program was written to evaluate and define optimum design parameters of low pressure auxiliary propulsion system. APS will provide attitude and translational control of space shuttle vehicles. Program evaluates subsystem design parameters such as engine chamber pressure, mixture ratio, expansion ratio, and subsystem component weight and size.


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    Title :

    Propulsion sizing program


    Contributors:

    Publication date :

    1972-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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