Research Catalog

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  • Simplified liquid oxygen propellant conditioning concepts [microform] / N.L. Cleary, K.A. Holt, and R.H. Flachbart.

    • Text
    • [Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Dynamic simulation of a wave rotor topped turboshaft engine [microform] / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Space shuttle hypergold load determination using nonintrusive ultrasonic flowmeters [microform] / Rudolph Werlink, Andrew Kelley, Ravi Margasahayam.

    • Text
    • Kennedy Space Center, Fla. : National Aeronautics and Space Administration, John F. Kennedy Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Arcjet thruster research and technology [microform] : phase I final report / [prepared by Seven C. Knowles].

    • Text
    • Cleveland, OH : NASA Lewis Research Center, [1987]
    • 1987

  • Detailed studies of aviation fuel flowability [microform] : final report / H.K. Mehta and R.S. Armstrong.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, 1985.
    • 1985

  • Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine / 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, October 1983.
    • 1983-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51158

  • Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine / 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, October 1983.
    • 1983-10

  • Impact of an exhaust throat on semi-idealized rotating detonation engine performance / Daniel E. Paxson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2016.
    • 2016-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68694

  • Dynamic simulation of a wave rotor topped turboshaft engine / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1997.
    • 1997-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo73175

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