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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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This slide presentation reviews the legacy of successes in the space shuttle program particularly with regards to the changes in the culture of NASA's organization after the Challenger and Columbia accidents and some of the changes to the shuttles that were made manifest as a result of the accidents..
Introductory information for equations to perform guidance, navigation, and control onboard computation functions for space shuttle orbiter
Initial data for space shuttle orbiter guidance, navigation, and control equations for preflight, boost, separation, orbit insertion, and ascent abort phases
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