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  • Conceptual design of an orbital debris defense system [microform].

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

  • A comparison of hypersonic vehicle flight and prediction results [microform] / Kenneth W. Iliff and Mary F. Shafer.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Convective and radiative heating for vehicle return from the Moon and Mars [microform] / R.B. Greendyke, P.A. Gnoffo.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • DSMC simulations of OREX entry conditions [microform] / James N. Moss, Roop N. Gupta, Joseph M. Price.

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

  • Synthesis of contributed simulations for OREX test cases [microform] / Unmeel B. Mehta.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Reentry-F flowfield solutions at 80,000 ft. [microform] / W.A. Wood, C.J. Riley, and F.M. Cheatwood.

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

  • Dynamic finite element predictions for Mars sample return cellular impact test #4 [microform] / Edwin L. Fasanella, Marcus D. Billings.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27476

  • Investigations of control surface seals for re-entry vehicles [microform] / Patrick H. Dunlap ... [et al.] ; [prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002

  • Investigations of control surface seals for re-entry vehicles [microform] / Dunlap, Patrick H. ; [prepared for 39th Joint Propulsion Conference and Exhibit ; cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS36329

  • Comparison of nonequilibrium solution algorithms applied to chemically stiff hypersonic flows [microform] / G. Palmer and E. Venkatapathy.

    • Text
    • Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54368

  • Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ [microform] / M. Leroy Spearman.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85587

  • Experiment module/support module interface specification for the reusable reentry satellite [microform] / prepared by Science Applications International Corporation.

    • Text
    • Torrance, Calif. : SAIC ; [Houston, Tex.] : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97533

  • Space Transfer Vehicle Concepts and Requirements Study. Volume II. Book 2. Appendix [microform].

    • Text
    • Denver, Colo. : Martin Marietta, Astronautics Group ; Huntsville, AL : NASA, Marshall Space Flight Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS98264

  • Outline for reusable reentry satellite system specification [microform] : volumes 1 - volume 9 / SAIC.

    • Text
    • Torrance, Calif. : Science Applications International Corporation ; Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS101374

  • Reusable Reentry Satellite (RRS) summary report [microform] : configuration trade study / prepared by SAIC.

    • Text
    • Torrance, Calif. : Science Applications International Corp. ; Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS101334

  • Reusable Reentry Satellite (RRS) summary report [microform] : launch tradeoff study / prepared by SAIC.

    • Text
    • Torrance, Calif. : Science Applications International Corporation ; Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS101371

  • Quasi non-intrusive sampling and analysis of gases associated with the boundary layer on the tethered satellite and similar supersonic and hypersonic research vehicles [microform] / by Charles Fishel, Stacie Niederriter, and Kenneth G. Brown (principal investigator) ; submitted by the Old Dominion University Research Foundation.

    • Text
    • Norfolk, Va. : Department of Chemical Sciences, School of Sciences and Health Professions, Old Dominion University, [1985]
    • 1985

  • Guidelines of the design of electropyrotechnic firing circuit for unmanned flight and ground test projects / Guillermo A. Gonzalez, Melvin H. Lucy, and Jeffrey J. Massie.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo45681

  • Reusable Reentry Satellite (RRS) summary report : propulsion system trade study.

    • Text
    • Torrance, California : Science Applications International Corporation, April 1990.
    • 1990-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54107

  • Reusable Reentry Satellite (RRS) summary report : propulsion system trade study.

    • Text
    • Torrance, Calif. : Science Applications International Corporation, April 1990.
    • 1990-4

  • Comparison of analysis with test for static loading of two hypersonic inflatable aerodynamic decelerator concepts / Karen H. Lyle.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2015.
    • 2015-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62835

  • An adaptive guidance algorithm for an aerodynamically assisted orbital plane change maneuver / James A Blissit Jr.

    • Text
    • Cambridge, Massachusetts : The Charles Stark Draper Laboratory, Inc, May 1986.
    • 1986-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo64996

  • An adaptive guidance algorithm for an aerodynamically assisted orbital plane change maneuver / James A Blissit Jr.

    • Text
    • Cambridge, Massachusetts : The Charles Stark Draper Laboratory, Inc, May 1986.
    • 1986-5

  • Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 / L. Roane Hunt.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71441

  • Numerical solutions of the Navier-Stokes equations for transonic afterbody flows / R. Charles Swanson, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71441

  • DSMC simulations of OREX entry conditions / James N. Moss, Roop N. Gupta, Joseph M. Price.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1996]
    • 1996
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79368

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