The purpose of this program was to develop a hot gas vane motor that would have application to advanced aircraft APU starting. Over the course of the program, the motor design evolved to the point that -65 degrees F starts, hot restarts above 130 degrees F, and multiple starts without refurbishment were possible. Analytical studies evaluated concepts for reducing motor internal friction. (Author)


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    Titel :

    Hydrazine APU Starter Development


    Beteiligte:
    D. A. Pahl (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    169 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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