A preliminary design for an unmanned hypersonic research vehicle to test scramjet engines is presented. The aircraft will be launched from a carrier aircraft at an altitude of 40,000 feet at Mach 0.8. The vehicle will then accelerate to Mach 6 at an altitude of 100,000 feet. At this stage the prototype scramjet will be employed to accelerate the vehicle to Mach 10 and maintain Mach 10 flight for 2 minutes. The aircraft will then decelerate and safely land.


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    Titel :

    OVRhyp, Scramjet Test Aircraft


    Beteiligte:
    Aslan, J. (Autor:in) / Bisard, T. (Autor:in) / Dallinga, S. (Autor:in) / Draper, K. (Autor:in) / Hufford, G. (Autor:in) / Peters, W. (Autor:in) / Rogers, J. (Autor:in)

    Erscheinungsdatum :

    1990-05-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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