Research Catalog

  • Shuttle flight data and in-flight anomaly list [microform] : STS-1 through STS-50, and STS-52 through STS-56 / prepared by Flight Requirements Support Section, Lockheed Engineering and Sciences Company.

    • Text
    • Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • Lightning threat analysis for the Space Shuttle Launch Pad and the payload changeout room using finite difference methods [microform] / prepared by Richard S. Collier.

    • Text
    • [Kennedy Space Center, Fla.] : National Aeronautics and Space Administration, John F. Kennedy Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • A model for Space Shuttle orbiter tire side forces based on NASA Landing Systems Research Aircraft test results [microform] / John F. Carter, Christopher J. Nagy, and Joseph S. Barnicki.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997
  • Development of the X-33 aerodynamic uncertainty model [microform] / Brent R. Cobleigh.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • STS-1 pogo analysis [microform].

    • Text
    • Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1981]
    • 1981
  • Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel [microform] / Paul M. Siemers, III and Martin W. Henry.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
  • Satellite services system program plan [microform] / [Stephen J. Hoffman].

    • Text
    • Schaumburg, IL : Advanced Planning and Analysis Division, Space Sciences Dept., Science Applications International Corporation ; Houston, Tex. : Engineering Directorate, NASA Lyndon B. Johnson Space Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88727
  • An investigation of selected on-orbit satellite servicing issues [microform] / [Stephen J. Hoffman].

    • Text
    • Schaumburg, IL : Advanced Planning and Analysis Division, Space Sciences Dept., Science Applications International Corporation ; Houston, TX : Engineering Directorate, NASA Lyndon B. Johnson Space Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88748
  • Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment [microform] / R. B. Miles, D. A. Santavicca, and M. Zimmermann.

    • Text
    • Princeton, N.J. : Princeton University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88186
  • Analytical prediction of aerothermal environment in a wing-elevon cove [microform] / Kim S. Bey.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983
  • In-flight load testing of advanced shuttle thermal protection systems [microform] / Bianca M. Trujillo, Robert R. Meyer, Jr., and Paul M. Sawko.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1983.
    • 1983
  • Study of several factors affecting crew escape trajectories from the space shuttle orbiter at low-subsonic speeds [microform] / William I. Scallion ... [et al.].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96456
  • Ground facilities for large space structures dynamics and control verification [microform] / Henry Waites.

    • 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/LPS104820
  • Orbiter-based construction equipment study [microform] : HPA/DTA technology advancement plan / prepared by Grumman Aerospace Corporation.

    • Text
    • Houston, TX : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1983]
    • 1983
  • Thermostructural evaluation of joggle region on the shuttle orbiter's wing leading edge / Sandra P. Walker and Jerry E. Warren.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo28056
  • Space shuttle orbiter trimmed center-of-gravity extension study. Volume ix. Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5 / W. Pelham Phillips and Roger H. Fournier.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January1985.
    • 1985-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo59036
  • Use of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations / Yehia M. Rizk, Joseph L. Steger, Denny S. Chausse.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, July 1985.
    • 1985-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo35006
  • A model for space shuttle orbiter tire side forces based on NASA landing systems research aircraft test results / John F. Carter, Christopher J. Nagy, and Joseph S. Barnicki.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, September 1997.
    • 1997-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66604
  • Compendium of information for interpreting the microgravity environment of the orbiter spacecraft / Richard DeLombard.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo66242
  • Development of the reentry flight dynamics simulator for evaluation of Space Shuttle Orbiter entry systems / Lawrence F. Rowell, Richard W. Powell, and Howard W. Stone, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1980.
    • 1980-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70979
  • Aerothermal analysis of a wing-elevon cove with variable leakage / L. Roane Hunt.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.
    • 1980-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71098
  • Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests / Delma C. Freeman, Jr., and Barnard Spencer, 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/gpo71431
  • Effects of experiment location and orbiter attitude on the residual acceleration on-board STS-73 (USML-2) / Roshanak Hakimzadeh [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79341
  • Materials testing on the DC-X and DC-XA / Dane Smith [and three others].

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, January 1997.
    • 1997-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69806
  • Extraction of stability and control derivatives from orbiter flight data / Kenneth W. Iliff and Mary F. Shafer.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1993.
    • 1993-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71191
  • Materials testing on the DC-X and DC-XA / Dane Smith [and three others].

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, January 1997.
    • 1997-1
  • Space shuttle orbiter trimmed center-of-gravity extension study : summary report / William I. Scallion and W. Pelham Phillips.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo93193
  • Preliminary mission designs for Jupiter orbiter missions / by Byron L. Swenson, Edward L. Tindle, and Larry A. Manning.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, May 1972.
    • 1972-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173284

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