This report summarizes the results of a United States Air Force funded effort to demonstrate the Multi-Axis Pintle Attitude Control (MAXPAC) system. The MAXPAC system is a spin-off of the Fourth Generation Escape Systems Technology Demonstration Program. MAXPAC uses four discrete, pintle-controlled rocket nozzles to provide variable thrust in three axes. The intent is to provide an under-seat retrofit for the Advanced Concept Ejection Seat (ACES) II replacing the current pitch stabilization rocket with the three-axis stabilization MAXPAC.


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    Titel :

    MAXPAC Test Program Final Presentation


    Beteiligte:
    J. Morris (Autor:in)

    Erscheinungsdatum :

    1996


    Format / Umfang :

    61 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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