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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Initial data for space shuttle orbiter guidance, navigation, and control equations for orbital operations of flight, rendezvous, docking, and stationkeeping
Low speed wind tunnel test on effects of horizontal tail geometry on longitudinal stability of orbiter shuttle
Aerodynamic forces and moments on orbiter and booster during space shuttle abort separation
Low speed aerodynamic characteristics of McDonnell Douglas scale model space shuttle booster
Hypervelocity wind tunnel tests of Convair B8B space shuttle booster and model configuration perturbations
Low speed wind tunnel tests of stability and control characteristics of space shuttle booster at subsonic speeds
Low speed wind tunnel tests on effects of vertical tail and geometry on directional stability of orbital space shuttle model
Low speed wind tunnel tests of subsonic aerodynamic properties of generic high cross range shuttle orbiter
Trisonic wind tunnel static stability tests on straight wing and delta wing space shuttle models
Trisonic wind tunnel stability tests on space shuttle modified orbiter model
Low speed wind tunnel tests of GAC 3A earth orbiting shuttle aerodynamic characteristics
Aerodynamic characteristics of GAC 518 earth orbital shuttle at Mach .170
Wind tunnel tests of lateral, longitudinal, and directional stability characteristics for scale model of orbiter shuttle
Subsonic aerodynamic characteristics of MDAC/MMC space shuttle booster configuration at Mach 0.26
Wind tunnel tests to determine static aerodynamic characteristics of space shuttle booster configuration at subsonic speeds
Wind tunnel tests to determine subsonic stability and control effectiveness of straight and delta wing configurations on space shuttle booster
Wind tunnel tests of delta wind and straight wing space shuttle orbiter models to determine static stability and control
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster proximity data, Mach number 5