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  • Heat flux measurement in SSME turbine blade tester [microform]/ Curt H. Liebert.

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

  • Performance improvement through indexing of turbine airfoils. Part 2, Numerical simulation [microform] / Lisa W. Griffin, Frank W. Huber and Om P. Sharma.

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

  • Simplified cyclic structural analyses of SSME turbine blades [microform] / A. Kaufman and J. M. Manderscheid.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • STS-1 pogo analysis [microform].

    • Text
    • Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1981]
    • 1981

  • SSME fuelside preburner two-dimensional analysis [microform] / Thomas J. Van Overbeke and Russell W. Claus.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Research pressure instrumentation for NASA space shuttle main engine [microform] : monthly report / prepared by P.J. Anderson, P. Nussbaum, G. Gustafson.

    • Text
    • Plymouth, MN : Honeywell Inc., Solid State Electronics Division, [1984]
    • 1984

  • Design study of magnetic eddy-current vibration suppression dampers for application to cryogenic turbomachinery [microform] : final report / E. J. Gunter, R.R. Humphris, and S. J. Severson.

    • Text
    • Charlottesville, Va. : University of Virginia, School of Engineering and Applied Science, Dept. of Mechanical and Aerospace Engineering, Rotor Dynamics Laboratory ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS86557

  • Bearing tester data compilation, analysis, and reporting and bearing math modeling [microform] : annual report.

    • Text
    • Huntsville, AL : SRS Technologies, Systems Technology Division, Aerospace and Commercial Systems Department ; [Marshall Space Flight Center, AL] : George C. Marshall Space Flight Center, [1986]
    • 1986

  • Distributed finite element analysis using a transputer network [microform] : final report / James Watson, ... [et al.].

    • Text
    • Huntsville, AL : SPARTA, Inc. ; Cleveland, OH : National Aeronautics and Space Administration, Lewis Research Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97610

  • In-house welding studies supporting the prelaunch assessment of the STS-6 main engines [microform] / by Lisa L. Hawkins.

    • Text
    • [ Huntsville, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1983]
    • 1983

  • 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

  • Flow processes in overexpanded chemical rocket nozzles. Part 1, Flow 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/LPS98683

  • Low loss injector for space shuttle main engine [microform] : final report / George L. von Pragenau.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99028

  • A computational study of multiple jet and wall interaction / Warren Campbell.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS105388

  • A computational study of multiple jet and wall interaction [microform] / Warren Campbell.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS105388

  • Space shuttle main engine vibration data base [microform] / Pat Lewallen.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104159

  • Statistical analysis of 59 inspected SSME HPFTP turbine blades (uncracked and cracked) [microform] / by John T. Wheeler.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104905

  • A review of the supply of liquid propellants and other fluids in support of the space shuttle program [electronic resource] / Stacy E. Churchwell.

    • Text
    • [Kennedy Space Center, Fla.] : National Aeronautics and Space Administration, John F. Kennedy Space Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108137

  • A review of the supply of liquid propellants and other fluids in support of the space shuttle program [microform] / Stacy E. Churchwell.

    • Text
    • [Kennedy Space Center, Fla.] : National Aeronautics and Space Administration, John F. Kennedy Space Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108137

  • Probabilistic structural analysis methods of hot engine structures [electronic resource] / C. C. Chamis and D. A. Hopkins.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108448

  • Probabilistic structural analysis methods of hot engine structures [microform] / C. C. Chamis and D. A. Hopkins.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108448

  • Analysis of internal flows relative to the space shuttle main engine [electronic resource] : final report.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center ; Marshall Space Flight Center, AL : National Aeronautics and Space Administration, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112289

  • Duct flow nonuniformities : effects of struts in SSME HGM II⁺ : interim report / prepared for National Aeronautics and Space Administration, Marshall Space Flight Center, by Roger Burke.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center ; Marshall Space Flight Center, AL : National Aeronautics and Space Administration, [1988]
    • 1988
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112315

  • Development of a computational aero/fluids analysis system [electronic resource] : final report / P. B. Kelley.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center ; Marshall Space Flight Center, AL : National Aeronautics and Space Administration, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112133

  • Analysis of internal flows relative to the space shuttle main engine [microform] : final report.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center ; Marshall Space Flight Center, AL : National Aeronautics and Space Administration, [1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112289

  • Duct flow nonuniformities [microform] : effects of struts in SSME HGM II⁺ : interim report / prepared for National Aeronautics and Space Administration, Marshall Space Flight Center, by Roger Burke.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center ; Marshall Space Flight Center, AL : National Aeronautics and Space Administration, [1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112315

  • Development of a computational aero/fluids analysis system [microform] : final report / by P.B. Kelley.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center ; Marshall Space Flight Center, AL : National Aeronautics and Space Administration, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112133

  • SSME technology test bed fast shutdown assessment [microform] : final report / prepared by A. Liebman, J. O. Vilja.

    • Text
    • Canoga Park, Calif. : Rockwell International, Rocketdyne Division ; [Washington, D.C. : National Aeronautics and Space Administration, 1988]
    • 1988

  • Investigation of weld joint detection capabilities of a coaxial weld vision system [microform] : interim report / by K. J. Gangl and J. L. Weeks.

    • Text
    • [Canoga Park, Calif.?] : Rockwell International, Rocketdyne Division, [1985]
    • 1985

  • Analytical and experimental investigation of rubbing interaction in labryinth seals for a liquid hydrogen fuel pump [microform] / by Francis X. Dolan, Francis E. Kennedy, Erland M. Schulson.

    • Text
    • [Hanover, N.H.] : Creare R&D Incorporated, [1984]
    • 1984

  • Analyses of physical-chemical processes governing SSME internal fluid flows [microform] : progress report for November 1984 / by A.K. Singhal ... [et al.] ; prepared for National Aeronautics and Space Administration, George C. Marshall Space Flight Center.

    • Text
    • [Huntsville, Ala.] : CHAM of North America, [1984]
    • 1984

  • Research pressure instrumentation for NASA space shuttle main engine [microform] : monthly report / prepared by P.J. Anderson, P. Nussbaum, G. Gustafson.

    • Text
    • Plymouth, MN : Honeywell Inc., Solid State Electronics Division, [1985]
    • 1985

  • Investigation of weld joint detection capabilities of a coaxial weld vision system : interim report / by K. J. Gangl and J. L. Weeks.

    • Text
    • [Canoga Park, Calif.?] : Rockwell International, Rocketdyne Division ; [Huntsville], Ala. : NASA-Marshall Space Flight Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo22013

  • SSME structural dynamic model development : phase II, final report / by M. J. Foley and V. L. Wilson.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Company, Inc, Huntsville Engineering Center : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo23654

  • Performance predictions for an SSME configuration with an enlarged throat / by G. R. Nickerson, L. D. Dang.

    • Text
    • Carson City, Nev. : Software and Engineering Associates, Inc. ; [Huntsville, Ala.] : George C. Marshall Space Flight Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24038

  • SSME structural dynamic model development [microform] : phase II, final report / by M. J. Foley and V. L. Wilson.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Company, Inc, Huntsville Engineering Center : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1985]
    • 1985

  • Performance predictions for an SSME configuration with an enlarged throat [microform] / by G. R. Nickerson, L. D. Dang.

    • Text
    • Carson City, Nev. : Software and Engineering Associates, Inc. ; [Huntsville, Ala.] : George C. Marshall Space Flight Center, [1985]
    • 1985

  • Turbomachinery incipient failure detection indicators and analysis / D.R. Faby, R.L. Smith, J.L. Frarey.

    • Text
    • Latham, N.Y. : Shaker Research Corporation ; [Huntsville, Ala.] : National Aeronautics & Space Administration, George C. Marshall Space Flight Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24077

  • Duct flow nonuniformities study for Space Shuttle main engine : technical report / by Jürgen Thoenes.

    • Text
    • Huntsville. AL : Lockheed, Missiles & Space Company. Inc, Huntsville Engineering Center ; National Aeronautics and Space Administration, Marshall Space Flight Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24279

  • Space Shuttle main engine (SSME) LOX turbopump pump-end bearing analysis : final report.

    • Text
    • Huntsville, Ala. : SRS Technologies, Systems Technology Division ; Marshall Space Flight Center, Ala. : Materials and Processes Laboratory, Engineering Physics Division, George C. Marshall Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24147

  • Engineering evaluation of SSME dynamic data from engine tests and SSV flights : final report / Wyle Laboratories research staff.

    • Text
    • [Huntsville, Ala.] : Wyle Laboratories, Scientific Services & Systems Group ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24421

  • Computational analysis of the SSME fuel preburner flow : final report / by Ten-See Wang, Richard C. Farmer.

    • Text
    • Huntsville, AL : Continuum, Inc. ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24431

  • A data base and analysis program for shuttle main engine dynamic pressure measurements : final report / by Thomas Coffin.

    • Text
    • [Huntsville, Ala.] : Wyle Laboratories Scientific Services & Systems Group ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24526

  • Investigation of breadboard temperature profiling system for SSME fuel preburner diagnostics : final technical report / J. A. Shirley.

    • Text
    • East Hartford, Conn. : United Technologies Research Center ; Marshall Space Flight Center, Ala. : George C. Marshall Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24466

  • Characterization of real gas properties for Space Shuttle main engine fuel turbine and performance calculations / Gary J. Harloff.

    • Text
    • Cleveland, Ohio : Sverdrup Technology, Inc., Lewis Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24991

  • Turbomachinery incipient failure detection indicators and analysis [microform] / D.R. Faby, R.L. Smith, J.L. Frarey.

    • Text
    • Latham, N.Y. : Shaker Research Corporation ; [Huntsville, Ala.] : National Aeronautics & Space Administration, George C. Marshall Space Flight Center, [1985]
    • 1985

  • Space Shuttle main engine (SSME) LOX turbopump pump-end bearing analysis [microform] : final report.

    • Text
    • Huntsville, Ala. : SRS Technologies, Systems Technology Division ; Marshall Space Flight Center, Ala. : Materials and Processes Laboratory, Engineering Physics Division, George C. Marshall Space Flight Center, [1986]
    • 1986

  • Duct flow nonuniformities study for Space Shuttle main engine [microform] : technical report / by Jürgen Thoenes.

    • Text
    • Huntsville. AL : Lockheed, Missiles & Space Company. Inc, Huntsville Engineering Center ; National Aeronautics and Space Administration, Marshall Space Flight Center, [1985]
    • 1985

  • Engineering evaluation of SSME dynamic data from engine tests and SSV flights [microform] : final report / Wyle Laboratories research staff.

    • Text
    • [Huntsville, Ala.]. : Wyle Laboratories, Scientific Services & Systems Group ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986

  • Computational analysis of the SSME fuel preburner flow [microform] : final report / by Ten-See Wang, Richard C. Farmer.

    • Text
    • Huntsville, AL : Continuum, Inc. ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986

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