Study relates geometry of an internally burning, single, solid-propellant grain to propellant characteristics, engine requirements, and selected starting pressure. Study derives curves for selecting propellants to meet specific engine requirements, or for tailoring engine requirements to propellant limitations.


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    Title :

    Starter propellants and auxiliary generators for gas turbines


    Contributors:
    Gill, G. S. (author)

    Publication date :

    1970-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


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