The Hyper-X Program, NASA's focused hypersonic technology program jointly run by NASA Langley and Dryden, is designed to move hypersonic, air-breathing vehicle technology from the laboratory environment to the flight environment, the last stage preceding prototype development. The Hyper-X research vehicle will provide the first ever opportunity to obtain data on an airframe integrated supersonic combustion ramjet propulsion system in flight, providing the first flight validation of wind tunnel, numerical and analytical methods used for design of these vehicles. A substantial portion of the integrated vehicle/engine flowpath development, engine systems verification and validation and flight test risk reduction efforts are experimentally based, including vehicle aeropropulsive force and moment database generation for flight control law development, and integrated vehicle/engine performance validation. The Mach 7 engine flowpath development tests have been completed, and effort is now shifting to engine controls, systems and performance verification and validation tests, as well as, additional flight test risk reduction tests.


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    Titel :

    Hyper-X Engine Design and Ground Test


    Beteiligte:
    R. T. Voland (Autor:in) / K. E. Rock (Autor:in) / L. D. Huebner (Autor:in) / D. W. Witte (Autor:in) / K. E. Fishcer (Autor:in)

    Erscheinungsdatum :

    2004


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hyper-X Engine Design and Ground Test Program

    Voland, R. T. / Rock, K. E. / Huebner, L. D. et al. | British Library Conference Proceedings | 1998


    Hyper-X Engine Design and Ground Test Program

    Voland, R. T. / Rock, K. E. / Huebner, L. D. et al. | NTRS | 1998


    Hyper-X engine design and ground test program

    Voland, R. / Rock, K. / Huebner, L. et al. | AIAA | 1998


    NASA's Hyper-X Scramjet Engine Ground Test Program

    Rock, K. E. / Voland, R. T. / Rogers, R. C. et al. | British Library Conference Proceedings | 1999


    Hyper-X Mach 7 Scramjet Design, Ground Test and Flight Results

    Ferlemann, Shelly M. / McClinton, Charles R. / Rock, Ken E. et al. | NTRS | 2005