A far ultraviolet polarization analyzer for rocket use
Far ultraviolet polarization analyzer for rocket measurement of resonantly scattered sunlight
ULTRAVIOLET LIGHT↗
SEARCH · Engineering Papers
Results for “Rocket”
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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Studies of the equatorial ionosphere using rocket techniques
Equatorial ionospheric propagation studies using rocket sounding techniques
MAGNETIC EQUATOR↗
Air shock parameters and design criteria for rocket explosions
Rocket explosion air blast parameters and design in relation to structural load calculations
ROCKET FIRING↗
Analytical investigation of key problems in the water-injection-cooled diffuser for nuclear rocket engine/stage test stands 2 - 3 Final report
Revised computer program on feasibility of water injection-cooled diffuser for nuclear rocket engine/stage test stands
NUCLEAR ROCKET↗
Experimental verification of a double-dead time model describing chugging in liquid bipropellant rocket engines
Experimental verification of double dead time model describing chugging in liquid bipropellant rocket engines
LIQUID PROPELLANT ROCKET ENGINE↗
Some injector element detail effects on screech in hydrogen-oxygen rockets
Concentric tube injection effect on dynamic characteristics of hydrogen-oxygen rocket
ROCKET THRUST↗
A theoretical study of nonlinear combustion instability in liquid propellant rocket engines.
Nonlinear combustion instability in liquid propellant rocket engines, describing nonsteady combustion process with aid of Crocco time-lag hypothesis
LIQUID PROPELLANT ROCKET ENGINE↗
Controlling the dimensions and orientation of impinging propellant sheets in liquid rocket engine injectors.
Working equations for dimensions and orientation of impinging propellant sheets in liquid rocket engine injectors
FUEL INJECTION↗
Dynamic performance of Surveyor throttleable rocket engine operating on propellants containing dissolved gas.
Surveyor throttleable liquid propellant rocket engine for operation on propellants saturated with dissolved liquid gas
HELIUM↗
Analysis and prediction of effects of exhaust products from aluminized solid-propellant rocket motors on launch facilities.
Effect on protective coatings of launch pads of exhaust products, chamber pressure, nozzle diameter, etc, from aluminized solid propellant rocket motors
PROTECTIVE COATING↗
Development and construction of Gerdien condenser rocket probes.
Mechanical construction of two types of Gerdien condenser rocket probes, noting instrumentation racks and inflatable parachutes for descent
INFLATABLE STRUCTURE↗
Sampling with a luster sounding rocket during a Leonid meteor shower.
Micrometeoroid sampling with Luster sounding rocket during Leonid meteor shower, detailing contamination control program
METEOR SHOWER↗
Transient heat transfer and thermal stresses for a nuclear rocket due to sudden increase of coolant flow.
Transient heat transfer and thermal stresses for nuclear rocket due to sudden hydrogen coolant flow increase
HYDROGEN↗
The ignition transient in solid propellant rocket motors.
Ignition pressure transient in solid rocket motors, examining chamber filling interval, flame propagation, heat transfer correlation, burning area, etc
TRANSIENT PRESSURE↗
Spectral radiance measurements of model rocket exhaust gases at simulated altitude, using a rapid scanning spectrometer.
Spectral radiance of model rocket exhaust gases measured by rapid scanning spectrometer at simulated altitude
EXHAUST GAS↗
External and Internal Air Loads on Sounding Rockets
Air loads on sounding rocket from distributed aerodynamics and pressure differential
SOUNDING ROCKET↗
Evaluation of error in application of WKB METHOD to linearized post burnout equation of motion of a sounding rocket.
Error in application of WKB method to linearized postburnout equation of motion of sounding rocket
SOUNDING ROCKET↗
Spin Acceleration Effects on Some Full-Scale Solid Rockets
Ballistic propellant combustion alteration and thermal effects due to dynamic spinning observed on solid propellant sounding rockets
SOLID PROPELLANT↗