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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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Deep-stall characteristics of T-tailed aircraft configurations and recovery procedures, noting parameters of pitch-up, angle of attack, etc
Liquid equilibrium configurations and disturbances of vehicle motion due to liquid sloshing in space
Effect of several injector face baffle configurations on screech in 20,000-lb thrust hydrogen-oxygen rocket
Beta hydroxyvaline synthesis, resolution and configuration
Optical resolution and configuration of trans-2, 3-epoxybutyric acid by brucine
Model testing for design evaluation of major components and configurations of static test and launch facilities, noting hot jet model
Forward facing jets effect on blunt configurations aerodynamic characteristics from wind tunnel tests at Mach 6, emphasizing drag increase
Equilibrium configuration and tension of flexible cable in uniform flow field, considering tangential drag force and weight effects
Optimum entry vehicle design using aerobreaking for manned earth entry at hyperbolic speeds, examining blunted conic, biconic and tetrahedral configurations
Zeeman effect of germanium I and II, discussing configuration-interaction, deriving intermediate- coupling wave functions
Effects of electric fields and configurations on thermal annealing and radiation hardening of MOSFETs
Anode heat transfer in MPD arc, discussing configurations and thrustors
Spiral arm magnetic field configuration model simplifies star formation theory, discussing theoretical and observational evidence
Oscillating mass flow characteristics in modified Moore variometer configuration for step, triangular and infrasonic functions
Spacecraft configurations and propulsion system module design for Voyager project, based on lunar module descent stage applications
Computer program for determining geometric configuration view factors for spherical and conical surfaces of spherical radiating bodies
Stability effects of several injector face baffle configurations on screech in hydrogen-oxygen rocket
Static longitudinal aerodynamic characteristics of configurations used in Little Joe/Apollo test vehicle development