SCALE MODEL TESTING OF 90 DEG TURN EJECTOR SYSTEMS FOR ROCKET ENGINE ALTITUDE SIMULATION
Scale model testing of 90 degree turn ejector systems for rocket engine altitude simulation
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Scale model testing of 90 degree turn ejector systems for rocket engine altitude simulation
Rocket extinction in vacuum environment, using regressive grains to determine low pressure limit for any propellant formation
Flight vibration data of aerobee 150a sounding rocket
Nike-apache sounding rocket - trajectory analysis
Electron density profiles for quiet day mid- latitude d region using nike-apache sounding rockets
Transonic and supersonic aerodynamic characteristics for two-stage rocket vehicle with blunted nose cone on square body with conical flare termination
Photography of earth surface from sounding rockets and satellites
Moderator wall cooling of high thrust cavity type gaseous nuclear rocket engines
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Control of absorption cross section of nuclear rocket with distributed parameter kinetics using two optimization procedures
Theoretical prediction of rolling motion of Nike-Cajun and Nike-Apache rocket vehicles
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Analytical and experimental studies of parachutes for deployment of meteorological instruments from sounding rockets
Performance of liquid hydrogen flow system during startup transient of nuclear rocket in full scale simulated engine system
Aerobee sounding rocket observation of very low frequency propagation and noise in ionosphere
Solid propellant composition and rocket motor design effect on plasma microwave and visible light attenuation emitted by exhaust
Viscoelastic analysis of structural integrity of accelerated ablating rocket
Nuclear rocket nozzle design using radiation cooling