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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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Ground proximity and ground-plane boundary layer effects on aerodynamic characteristics of four-propeller tilt-wing V/STOL configuration
Formula derivation for optimum satellite station configurations for simultaneous direction observations to satellites
Compilation of wind-tunnel heat-transfer measurements on afterbody of Mercury capsule reentry configuration
Lateral and longitudinal aerodynamic characteristics of hypersonic missile configurations with canard controls in supersonic pressure tunnel
Comparison of flight measured carrier-approach speeds with values predicted by several different criteria for 41 fighter aircraft configurations
Pressure distribution on hypersonic glide configuration having 79.5 deg sweepback and 45 deg dihedral at Mach number of 4.95
Static aerodynamic characteristics of modified Mercury exit and escape capsule configurations at Mach numbers 3.0 to 6.8
Wind tunnel testing of dorsal-fin, delta-wing and dart-wing configurations
Configuration modifications of tension shell shapes to improve aerodynamic characteristics at Mach 3 by delaying onset of flow separation
Helical instability of positive column in crossed fields and in annular plasma configurations
Analytical evaluation of aerodynamic load growth or steady state aeroelastic effect for Saturn configurations
Far-field acoustic environmental predictions for launch of Saturn V and Saturn V MLV CONFIGURATION
Extension of configuration management techniques to computer programming
Simulated air speed control system to investigate overspeeding and maneuver speed of supersonic transport configuration in relation to speed margin
Flight simulator study of pitch maneuver speed margins for variable-sweep wing supersonic transport configuration
Power system configurations and reliability for interplanetary missions to Mercury, Venus, Mars, and Jupiter
Configuration identification data and management procedures for Voyager project
Wind tunnel measurements on two wing-end plate aircraft model configurations