The Hybrid Propulsion Demonstration Program (HPDP) program was formed to mature hybrid propulsion technology to a readiness level sufficient to enable commercialization for various space launch applications. The goal of the HPDP was to develop and test a 250,000 pound vacuum thrust hybrid booster in order to demonstrate hybrid propulsion technology and enable manufacturing of large hybrid boosters for current and future space launch vehicles. The HPDP has successfully conducted four tests of the 250,000 pound thrust hybrid rocket motor at NASA's Stennis Space Center. This paper documents the test series.


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    Titel :

    Hybrid Propulsion Demonstration Program 250K Hybrid Motor


    Beteiligte:
    Story, George (Autor:in) / Zoladz, Tom (Autor:in) / Arves, Joe (Autor:in) / Kearney, Darren (Autor:in) / Abel, Terry (Autor:in) / Park, O. (Autor:in)

    Kongress:

    39th AIAA/ISME/ASEE Joint Propulsion Conference and Exhibit ; 2003 ; Huntsville, Al, United States


    Erscheinungsdatum :

    23.07.2003


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hybrid Propulsion Demonstration Program 250K Hybrid Motor

    G. Story / T. Zoladz / J. Arves et al. | NTIS | 2003


    Hybrid Propulsion Demonstration Program 250K Hybrid Motor

    Story, George / Abel, Terry / Claflin, Scott et al. | AIAA | 2003


    Hybrid Propulsion Demonstration Program 250K Hybrid Motor

    Story, G. / Zoladz, T. / Arves, J. et al. | British Library Conference Proceedings | 2003


    Performance analyses of HPDP 250K hybrids

    Park, O. / Bryant, C. / Carpenter, R. | AIAA | 2000


    Performance Analyses of HPDP 250K Hybrids

    Park, O. Y. / Bryant, C. T. / Carpenter, R. L. et al. | British Library Conference Proceedings | 2000