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  • Final report for the NASA reload program [microform] / submitted by Atlantic Research Corporation.

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

  • Final postflight hardware evaluation report, 360T021 (RSRM-21, STS-45) [microform].

    • Text
    • Brigham City, Utah : Thiokol Corp., Space Operations ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners [microform] / Vinod K. Arya and Gary R. Halford.

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

  • 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

  • Star 48 solid rocket motor nozzle analyses and instrumented firings [microform] / Robert L. Porter.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
    • 1986

  • High performance solid rocket motor (SRM) submerged nozzle-combustion cavity flowfield assessment [microform] : final report / prepared by J.A. Freeman ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center [microform] / Kenneth J. Davidian, Ronald H. Dieck and Isaac Chuang ; prepared for the 24th JANNAF Combustion Meeting, Monterey, California, October 5-9, 1987.

    • Text
    • [Washington, D.C.?] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Advanced small rocket chambers option 3 [microform] : 110 1bf Ir-Re rocket / Donald M. Jassowski and Leonard Schoenman.

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

  • A performance comparison of two small rocket nozzles [microform] / Lynn A. Arrington, Brian D. Reed, Angel Rivera, Jr.

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

  • Multidisciplinary approach to aerospike nozzle design [microform] / J.J. Korte ... [et al.].

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

  • Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure [microform] / M. Moin Hussaini and John J. Korte.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure [microform] / Robert S. Jankovsky and John M. Kazaroff, Albert J. Pavli.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis [microform] / Timothy D. Smith ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle [microform] / Timothy W. Simpson.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation [microform] / Robert S. Jankovsky and Timothy D. Smith, Albert J. Pavli.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Development of thermal barriers for solid rocket motor nozzle joints [microform] / Bruce M. Steinetz, Patrick H. Dunlap, Jr.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • 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

  • Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 [microform] / George T. Carson, Jr., and Milton Lamb.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988.
    • 1988

  • RSRM nozzle fixed housing cooldown test final report [microform] / prepared by D. J. Bolieau.

    • Text
    • Brigham City, Utah : Morton Thiokol, Inc., Aerospace Group ; [Washington, D.C. : National Aeronautics and Space Administration, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68324

  • Shelf life extension for the lot AAE nozzle severance LSCs [micorform] : final test report / [prepared by M. Cook].

    • Text
    • Brigham City, UT : Thiokol Corp., Space Operations ; [Marshall Space Flight Center, Ala.. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center?, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70070

  • Flight motor set 360L002 (STS-27R). Volume 5, Nozzle component [microform] : final report / [prepared by S.A. Meyer].

    • Text
    • Brigham City, UT : Thiokol Corp., Space Operations ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70026

  • Flow processes in overexpanded chemical rocket nozzles. Part 2, Side loads due to asymmetric separation [microform] / Robert H. Schmucker.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS98675

  • Development of a high power microwave thruster, with a magnetic nozzle, for space applications / John L. Power and Randall A. Chapman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS107986

  • Development of a high power microwave thruster, with a magnetic nozzle, for space applications [microform] / John L. Power and Randall A. Chapman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS107986

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

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

  • Improved two-dimensional-kinetics computer program [microform] : second quarterly progress report, 1 April 1984 through 30 June 1984 / prepared by Gary R. Nickerson.

    • Text
    • Santa Ana, Calif. : Software and Engineering Associates, Inc. ; [Washington, D.C. : National Aeronautics and Space Administration, 1984?]
    • 1984

  • Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed / Daniel S. Jones [and four others].

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo58350

  • A performance comparison of two small rocket nozzles / Lynn A. Arrington, Brian D. Reed, Angel Rivera, Jr.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67112

  • Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure / M. Moin Hussaini and John J. Korte.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS67205

  • Compact fuel element environment test / D.E. Bradley [and three others].

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37675

  • Nuclear rocket propulsion [by] R.W. Bussard and R.D. De Lauer.

    • Text
    • New York, McGraw-Hill, 1958.
    • 1958
    • 1 Item
    FormatCall NumberItem Location
    Text TL783.5 .B8Off-site

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