02627oam 2200673 450 991070743950332120160825111517.0(CKB)5470000002465134(OCoLC)761092058(EXLCZ)99547000000246513420111115j198012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierComparison 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[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,December 1980.1 online resource (33 pages) illustrationsNASA technical paper ;1779Title from title screen (viewed on Aug. 25, 2016)."December 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 8).AileronsnasatApproach and landing tests (STS)nasatElevonsnasatLateral stabilitynasatLongitudinal stabilitynasatSpace Shuttle orbitersnasatArtificial satellitesOrbitsfastSpace vehiclesLandingfastStability of space vehiclesfastWind tunnelsGround simulatorsfastAilerons.Approach and landing tests (STS)Elevons.Lateral stability.Longitudinal stability.Space Shuttle orbiters.Artificial satellitesOrbits.Space vehiclesLanding.Stability of space vehicles.Wind tunnelsGround simulators.Freeman Delma C.1387391Spencer Bernard1932-Langley Research Center,United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOGPOBOOK9910707439503321Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests3440830UNINA