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Thursday, July 23, 2020 | History

2 edition of Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 found in the catalog.

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86

Milton Lamb

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86

by Milton Lamb

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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:
  • Guided missiles -- Control systems -- Testing.,
  • Guided missiles -- Aerodynamics -- Testing.,
  • Wind tunnels -- Testing.

  • Edition Notes

    StatementMilton Lamb.
    SeriesNASA technical memorandum -- 83223.
    ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Langley Research Center.
    The Physical Object
    Pagination116 p. :
    Number of Pages116
    ID Numbers
    Open LibraryOL17799132M


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Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 by Milton Lamb Download PDF EPUB FB2