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Wednesday, August 12, 2020 | History

2 edition of Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63 found in the catalog.

Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63

Delma C. Freeman

Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63

by Delma C. Freeman

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Published by National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Information Service in [Washington], Springfield, Va .
Written in English

    Subjects:
  • Stability of space vehicles.

  • Edition Notes

    StatementDelma C. Freemand, Jr. and Roger H. Fournier.
    SeriesNASA technical memorandum ; 74056, NASA technical memorandum -- 74056.
    ContributionsFournier, Roger H., United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
    The Physical Object
    Pagination66 p. :
    Number of Pages66
    ID Numbers
    Open LibraryOL17647279M


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Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63 by Delma C. Freeman Download PDF EPUB FB2