Research Catalog

  • Carbon monoxide and oxygen combustion experiments [microform] : a demonstration of Mars in situ propellants / Diane L. Linne.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
  • Ignition and combustion characteristics of metallized propellants [microform] : phase II, annual report (June 1993-June 1994) / prepared by D.C. Mueller and S.R. Turns.

    • Text
    • University Park, PA : Dept. of Mechanical Engineering, Propulsion Engineering Research Center, Pennsylvania State University ; [Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Theoretical and experimental investigations of ignition, combustion, and expansion processes of hypergolic liquid fuel combinations at gas temperatures up to 3000⁰K [microform] / Harry Schulz.

    • Text
    • Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • Questions of testing rate and flexibility of rocket test benches [microform] : discussed on the basis of the test benches of nitrochemie GMBH in Aschau / Legrand.

    • Text
    • [Redwood City, Calif. : Leo Kanner Associates] ; Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • Propellant injection systems and processes [microform] / Jackson I. Ito.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Metallized gelled propellants [microform] : oxygen/RP-1/aluminum rocket combustion experiments / Bryan Palaszewski and James S. Zakany.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Fundamental phenomena on fuel decomposition and boundary layer combustion processes with applications to hybrid rocket motors [microform] : semi-annual report / Kenneth K. Kuo ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995-
    • 1995-present
  • Hybrid fuel formulation and technology development [microform]: final report / prepared by David L. Dean.

    • Text
    • Huntsville, AL : McDonnell Douglas ; [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Long life testing of oxide-coated iridium/rhenium rockets [microform] / Brian D. Reed.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Testing of wrought iridium/chemical vapor deposition rhenium rocket [microform] / Brian D. Reed and Steven J. Schneider.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept [microform] / M.M. Fazah and J.M. Cramer.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Turbine engine hot section technology 1986 [microform] : proceedings of a conference / sponsored by NASA Lewis Research Center, Cleveland, Ohio, October 21 and 22, 1986.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54929
  • Fuel-rich catalytic combustion of a high density fuel [microform] / Theodore A. Brabbs, Sylvia A. Merritt.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service, 1993]
    • 1993
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60772
  • Study of basic physical processes in liquid rocket engines / by S.T. Wu and C.P. Chen.

    • Text
    • Huntsville, AL : NASA/Marshall Space Flight Center, September 1992.
    • 1992-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo174437
  • Study of basic physical processes in liquid rocket engines [microform] / by S.T. Wu and C.P. Chen.

    • Text
    • Huntsville, AL : NASA/Marshall Space Flight Center, September 1992.
    • 1992-9
  • Numerical analysis of a rotating detonation engine in the relative reference frame / Daniel E. Paxson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2014.
    • 2014-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57039
  • Thruster injector faceplate testing in support of the aerojet rocket-based combined cycle (RBCC) concept / M.M. Fazah and J.M. Cramer.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, May 1998.
    • 1998-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83111

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