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  • Design review and analysis for a Pratt & Whitney fluid-film bearing and seal testing rig [microform] : final report / by Dara W. Childs.

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

  • Sliding seal materials for Adiabatic engines [microform] : phase II interim report / James Lankford and William Wei.

    • Text
    • Washington, D.C. : U.S. Dept. of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Sliding seal materials for Adiabatic engines [microform] : phase I interim report / James Lankford.

    • Text
    • Washington, D.C. : U.S. Dept. of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1985]
    • 1985

  • Thermomechanical behavior of plasma-sprayed ZrO₂-Y₂O₃ coatings influenced by plasticity, creep and oxidation [microform] / J. Padovan ... [et al.].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92376

  • A dynamic analysis of rotary combustion engine seals [microform] / J. Knoll ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS98747

  • Experimental study of ceramic-coated tip seals for turbojet engines [microform] / T. J. Biesiadny, ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Cleveland, Ohio : Propulsion Laboratory, AVSCOM Research and Technology Laboratories, 1985]
    • 1985

  • Ribbon-burner simulation of the T-700 turbine shroud section for ceramic-lined seals research [microform] / J.K. Little ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104768

  • Block II solid rocket motor (SRM) conceptual design study : final report / submitted by Atlantic Research Corporation, Propulsion Division.

    • Text
    • Gainesville, Va. : Atlantic Research Corporation, Propulsion Division ; [Washington, D.C.] : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986-
    • 1986-present
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112826

  • 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

  • Experimental assessment of advanced Stirling component concepts [microform] / B. Ziph ; prepared for National Aeronautics and Space Administration, Lewis Research Center for U.S. Department of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D. under interagency agreement DE-A101-77CS51040.

    • Text
    • Ann Arbor, MI. : Stirling Thermal Motors, Inc. ; Washington, D.C. : U.S. Dept. of Energy, [1985]
    • 1985

  • SSME seal test program : test results for sawtooth-pattern damper seal : interim progress report / prepared by Dara W. Childs.

    • Text
    • College Station, Tex. : Turbomachinery Laboratories, Mechanical Engineering Dept., Texas A & M University ; [Washington, D.C.] : [National Aeronautics and Space Administration], [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24439

  • SSME seal test program [microform] : test results for sawtooth-pattern damper seal : interim progress report / prepared by Dara W. Childs.

    • Text
    • College Station, Tex. : Turbomachinery Laboratories, Mechanical Engineering Dept., Texas A & M University ; [Washington, D.C. : National Aeronautics and Space Administration], [1986]
    • 1986

  • Computational fluid mechanics utilizing the variational principle of modeling damping seals / by Continuum, Inc.

    • Text
    • Huntsville, AL : Continuum, Inc., April 10, 1984.
    • 1984-410
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo58880

  • Computational fluid mechanics utilizing the variational principle of modeling damping seals / by Continuum, Inc.

    • Text
    • Huntsville, AL : Continuum, Inc., April 10, 1984.
    • 1984-410

  • Effects of compression, staging, and braid angle on braided rope seal performance / Bruce M. Steinetz and Michael L. Adams.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo73164

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