Integrated propulsion control system for ramjet Hypersonic Research Engine to operate at 3-8 Mach numbers


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    Title :

    Hypersonic research engine integrated propulsion control.


    Contributors:
    Colwill, T. (author) / Curran, W. (author) / Stiglic, P. (author)

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE ; 1969 ; COLORADO SPRINGS, COLO.


    Publication date :

    1969-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Hypersonic research engine integrated propulsion control

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