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  • A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis [microform] / Kenneth J. Kacynski, John M. Kazaroff, and Robert S. Jankovsky.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • 7.5K lbf thrust engine preliminary design for orbit transfer vehicle [microform] : task D.5 final report / Warren R. Hayden, Ralph Sabiers, and Judy Schneider.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios [microform] / Kenneth J. Kacynski and Joe D. Hoffman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Integrated hydrogen-oxygen technology applied to auxilliary propulsion systems [microform] : final report / Rockwell International.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • A unique high heat flux facility for testing hypersonic engine components [microform] / Matthew E. Melis and Herbert J. Gladden.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Determination of the relative resistance to ignition of selected turbopump materials in high-pressure, high-temperature, oxygen environments [microform] : test report.

    • Text
    • Las Cruces, N.M. : Lyndon B. Johnson Space Center, White Sands Test Facility : [Washington, D.C. : National Aeronautics and Space Administration, ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle [microform].

    • Text
    • [West Palm Beach, Fla. : Pratt and Whitney Aircraft ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Predicted performance of an integrated modular engine system [microform] / Michael Binder and James L. Felder.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Dual-throat thruster thermal model [microform] : final report / by R.L. Ewen, C.J. O'Brien, and L.W. Matthews.

    • Text
    • Sacramento, Calif. : Aerojet TechSystems Co. ; [Huntsville, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center, Alabama ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Space Transportation Booster Engine (STBE) configuration study [microform] : second quarterly review.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • A transient model of the RL10A-3-3A rocket engine [microform] / Michael P. Binder.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Highly Evolved Expendable Launch Vehicle (HEELV) for the HRST program [microform] : final report, contract H27831D, W-6-PP-02996.

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

  • NASA flow field analysis [microform] : final report / Charles L. Merkle.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Qualitative flow visualization of a 110-N hydrogen/oxygen laboratory model thruster [microform] / Wim A. de Groot, Thomas J. McGuire, Steven J. Schneider.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Space station hydrogen/oxygen thruster technology / G.L. Briley and R.S. Iacabucci.

    • Text
    • [Cleveland, Ohio] : [National Aeronautics and Space Administration, Lewis Research Center], [1988]
    • 1988
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS47226

  • A comparison of analytical results for 20 K LOX/hydrogen instabilities [microform] / Mark D. Klem and Kevin J. Breisacher ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990?]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59891

  • Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines [microform] : phase I, final report / Jerry W. Brockmeyer and Gary D. Schnittgrund.

    • Text
    • Canoga Park, CA : Rocketdyne Division, Rockwell International ; Cleveland. Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69837

  • Retardation analytical model to extend service life [microform] : monthly technical progress narrative, month of August 1984 / prepared for National Aeronautics & Space Administration, Marshall Space Flight Center ; prepared by D. Matejczyk.

    • Text
    • Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [1984]
    • 1984

  • Configuration evaluation and criteria plan. Vol.2, Evaluation criteria plan (preliminary), space transportation main engine (STME) configuration study [microform] / prepared by E. K. Bair.

    • Text
    • Sacramento, Calif. : Aerojet TechSystems Co. ; Mashall Space Flight Center, Ala. : NASA George C. Marshal Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS93142

  • SPE® propulsion electrolyzer for NASA's integrated propulsion test article [microform] : final report / prepared by Hamilton Standard Division, Space & Sea Systems Department, Electro-Chem Programs.

    • Text
    • [Houston, Tex.] : National Aeronautics and Space Administration, Johnson Space Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS101785

  • Advanced research and technology programs for advanced high-pressure oxygen-hydrogen rocket propulsion / S.J. Marsik and S.F. Morea.

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS105610

  • Advanced research and technology programs for advanced high-pressure oxygen-hydrogen rocket propulsion [microform] / S.J. Marsik and S.F. Morea.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS105610

  • Turbine blade thermal fatigue testing Pratt and Whitney aircraft hollow core blades [microform] / by Jeff Ingram and Loren Gross.

    • Text
    • [Marshall Space Flight Center, Ala.?] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1985]
    • 1985

  • Perormance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydorgen-oxygen rocket [microform] / Lynn A. Arrington and Brian D. Reed.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1992?]
    • 1992

  • Configuration evaluation and criteria plan. Vol.1, System trades study and design methodology plan (preliminary), space transportation main engine (STME) configuration study [microform] / prepared for NASA George C. Marshall Space Flight Center.

    • Text
    • Sacramento, Calif. : Aerojet TechSystems Co. ; Mashall Space Flight Center, Ala. : NASA George C. Marshal Space Flight Center, [1986]
    • 1986

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