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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    Title :

    MAXPAC Test Program Final Presentation


    Contributors:
    J. Morris (author)

    Publication date :

    1996


    Size :

    61 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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