An over view of research into a low cost hypersonic research flight test capability to increase the amount of hypersonic flight data to help bridge the large developmental gap between ground testing/analysis and major flight demonstrator Xplanes is provided. The major objectives included: develop an air launched missile booster research testbed; accurately deliver research payloads through programmable guidance to hypersonic test conditions; low cost; a high flight rate minimum of two flights per year and utilize surplus air launched missiles and NASA aircraft.


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    Titel :

    Phoenix Missile Hypersonic Testbed (PMHT): Project Concept Overview


    Beteiligte:

    Kongress:

    SAE Aerospace Control and Guidance Systems Committee Meeting #99 ; 2007 ; Boulder, CO, United States


    Erscheinungsdatum :

    2007-03-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    The Pedestrian PMHT

    Efe, M. / Willett, P. / International Society of Information Fusion et al. | British Library Conference Proceedings | 2002


    The turbo PMHT

    Yanhua Ruan, / Willett, P. | IEEE | 2004


    The pedestrian PMHT

    Efe, M. / Ruan, Y. / Willett, P. | IEEE | 2002