The objective of this design project is to develop the hypersonic reconnaissance aircraft to replace the SR-71 and to complement existing intelligence gathering devices. The initial design considerations were to create a manned vehicle which could complete its mission with at least two airborne refuelings. The aircraft must travel between Mach 4 and Mach 7 at an altitude of 80,000 feet for a maximum range of 12,000 nautical miles. The vehicle should have an air breathing propulsion system at cruise. With a crew of two, the aircraft should be able to take off and land on a 10,000 foot runway, and the yearly operational costs were not to exceed $300 million. Finally, the aircraft should exhibit stealth characteristics, including a minimized radar cross-section (RCS) and a reduced sonic boom. The technology used in this vehicle should allow for production between the years 1993 and 1995.


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    Titel :

    Advanced hypersonic aircraft design


    Beteiligte:
    Utzinger, Rob (Autor:in) / Blank, Hans-Joachim (Autor:in) / Cox, Craig (Autor:in) / Harvey, Greg (Autor:in) / Mckee, Mike (Autor:in) / Molnar, Dave (Autor:in) / Nagy, Greg (Autor:in) / Petersen, Steve (Autor:in)

    Erscheinungsdatum :

    01.06.1992


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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