This program was initiated by the Air Force Rocket Propulsion Laboratory to demonstrate the flexible exit cone omniaxis movable nozzle concept by rocket motor testing. Program objectives are as follows: develop flexible exit cone design and criteria, perform a TVC system comparison, and demonstrate the flexible exit cone nozzle performance on four AFRPL 36 in. diameter char motor static tests with vectoring. (Author)


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    Titel :

    Flexible Exit Cone Nozzle Development Program


    Beteiligte:
    J. W. Wilson (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    109 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Flexible Exit Cone Nozzle Demonstration Firing Results

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