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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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Static aerodynamic characteristics of modified mercury escape and exit capsule configurations at mach numbers 0.30 to 1.4
Monte carlo computer technique applied to focusing of cryopump configurations in free molecular flow region
Rolling motion of 79-deg clipped delta wing configuration at supersonic speed - free flight investigation
Effect of contact angle and space vehicle tank geometry on configuration of rocket propellant liquid-vapor interface during weightlessness
Optimization of aft configuration of passive-entry capsule
Study of delta-wing configurations for supersonic transport application and their relation to aircraft performance
Design configurations for orbiting space stations
Results of experimental and analytic studies of delta-wing supersonic transport configurations
Dependence of sonic boom overpressures on supersonic aircraft configurations and design aspects to minimize boom
Application of low drag-due-to-lift concept of linearized theory to the studies of twist and camber of isolated wing and wing-body configurations of supersonic aircraft
Aerodynamic hinge moments caused by external flow on saturn i, block i nozzle configurations
Low-subsonic flight characteristics of model supersonic aircraft configuration with parawing as a landing aid
Effects of three dimensional roughness trips on aerodynamic characteristics and boundary layer transition of wing-body-tail configuration
Takeoff performance of supersonic transport configurations
Low-speed longitudinal aerodynamic investigation of parawings as auxiliary lifting devices for supersonic aircraft configuration
Wind tunnel and flight testing of airplane configuration influence on sonic boom characteristics
Aerodynamic characteristics of general & specific lifting & nonlifting configurations at mach 24
Store pitch flexibility effect on flutter characteristics of wing-store configurations in transonic wind tunnel