Rocket sounding of the upper atmosphere.
Different rockets with various payload capabilities for specific upper atmospheric investigations
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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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Different rockets with various payload capabilities for specific upper atmospheric investigations
Rocket and satellite investigations of ionospheric electron and ion collision frequencies, solar radiation, D, E and F regions, plasma frequency probe, etc
Liquid-core reactor concept examined for nuclear rocket
Optimization of supersonic portion of three- dimensional flow geometry in rocket motor nozzle for maximum thrust
Acoustic absorption liners for suppressing HF COMBUSTION instability in rocket engine combustion chambers
Digital computer technique for analysis of radiological hazards of nuclear rocket flight operations
Bray sudden freezing criterion for predicting nonequilibrium performance in multireaction liquid rocket nozzle expansion
Circulation system movement at various stratospheric and mesospheric levels based on rocket-grenade experiments
Rocket-nozzle environment simulation with DC arc- plasma generator noting graphite and phenolic material test results
Transient pressure measurements in rocket thrust chambers used in propulsion systems research
Rockets, satellites and space probe roles in atmospheric electricity research
TIROS and Nimbus meteorological satellites, and small and large meteorological sounding rocket experiments
Rocket performance parameter calculations based on equilibrium composition of combustion products
Hopi-Dart and Cajun-Dart rocket wind measuring systems
Vortex amplifier for controlling secondary flow for thrust vector control of liquid rocket engine
Photograph interpretation of V-2, Viking, and Aerobee rocket photography
IQSY rocket measurements in C, D, and E layers of ionosphere - electron density, collision frequency, molecular oxygen density, and ionization
Bending vibration equations for rocket boosted vehicle controlled by vectored thrust - structural dynamics