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Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests

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Freeman, Delma C., author Langley Research Center, author

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Title from title screen (viewed on Aug. 25, 2016)."December 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 8).Technical paper.National Aeronautics and Space Administration506-51-33-02L-13945
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Text
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Language Material Electronic Resource Computer Online Resource
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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body
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Pursuant to Title 17 Section 105 of the United States Code, this file is not subject to copyright protection and is in the public domain. For more information please see http://www.gpo.gov/help/index.html#public_domain_copyright_notice.htm
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United States Government Publishing Office (GPO)

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United States Government Publishing Office (GPO)

Keywords

  1. Ailerons
  2. Approach And Landing Tests (Sts)
  3. Artificial Satellites
  4. Elevons
  5. Ground Simulators
  6. Landing
  7. Lateral Stability
  8. Longitudinal Stability
  9. Orbits
  10. Space Shuttle Orbiters
  11. Space Vehicles
  12. Stability Of Space Vehicles
  13. Wind Tunnels

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