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  • Cg/stability map for the reference H cycle 3 supersonic transport concept along the high speed research baseline mission profile [microform] / Daniel P. Giesy and David M. Christhilf.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Space shuttle orbiter trimmed center-of-gravity extension study [microform] : summary report / William I. Scallion and W. Pelham Phillips.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • Determination of shuttle orbiter center of gravity from flight measurements [microform] / E. W. Hinson, J. Y. Nicholson, R. C. Blanchard.

    • Text
    • Hampton, Va. : NASA Langley Research Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60549

  • Weight and balance for the Airmass Incorporated Sunburst Model C ultralight / Jahn A. Woltkamp, project engineer; Carlos L. Blacklock, project manager; Dr. Jan Roskam, principal investigator.

    • Text
    • Lawrence, Kansas : Flight Research Laboratory, University of Kansas Center for Research, Inc. ; [Hampton, Va.] : National Aeronautics and Space Administration, Langley Research Center, November 1983.
    • 1983-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51157

  • Weight and balance for the Airmass Incorporated Sunburst Model C ultralight / Jahn A. Woltkamp, project engineer; Carlos L. Blacklock, project manager; Dr. Jan Roskam, principal investigator.

    • Text
    • Lawrence, Kansas : Flight Research Laboratory, University of Kansas Center for Research, Inc. ; [Hampton, Virginia] : National Aeronautics and Space Administration, Langley Research Center, November 1983.
    • 1983-11

  • Space shuttle orbiter trimmed center-of-gravity extension study. Volume ix. Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5 / W. Pelham Phillips and Roger H. Fournier.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January1985.
    • 1985-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo59036

  • Space shuttle orbiter trimmed center-of-gravity extension study : summary report / William I. Scallion and W. Pelham Phillips.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, 1985.
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo93193

  • Static controls performance tool for lunar landers / Eliot D. Aretskin-Hariton [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2018.
    • 2018-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo111588

  • Design status of Gondola for High-Altitude Planetary Science (GHAPS) / Robert Tornabene [and nine others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2023.
    • 2023-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo221052

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