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Saturday, October 31, 2020 | History

2 edition of Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86 found in the catalog.

Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86

Gregory D. Riebe

Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86

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  • 33 Currently reading

Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

    Subjects:
  • Aerodynamics, Supersonic.,
  • Winged spacecraft.

  • Edition Notes

    StatementGregory D. Riebe, William J. Small, and Odell A. Morris.
    SeriesNASA technical paper -- 1888.
    ContributionsSmall, William J. 1939-, Morris, Odell A., Langley Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
    The Physical Object
    Pagination52 p. :
    Number of Pages52
    ID Numbers
    Open LibraryOL17827734M


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Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86 by Gregory D. Riebe Download PDF EPUB FB2

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