Analysis of nonconstant area combustion and mixing in ramjet and rocket-ramjet hybrid engines
One-dimensional analysis of variable area mixing and combustion process in supersonic ramjet and rocket-ramjet hybrid engines
HYBRID ROCKET↗
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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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Some factors influencing heat transfer to liquid-propellant rocket-thrust-chamber coolant channels
Wall temperature and heat transfer patterns in liquid-propellant rocket thrust chamber coolant channels
LIQUID PROPELLANT ROCKET ENGINE↗
Experimental evaluation of throat inserts in a storable-propellant rocket engine
Evaluation of erosion resistant materials for throat inserts of ablative nozzle sections in storable propellant rocket engine
ABLATING MATERIAL↗
Analysis of Topping and Bleed Turbopump Units for Hydrogen-propelled Nuclear Rockets
Topping and bleed turbopump unit for hydrogen propelled nuclear rocket
NUCLEAR ROCKET↗
Transient Dynamics and Thermal Stress for Nuclear Rocket Heat-exchanger
Transient dynamics and thermal stresses in nuclear rocket heat exchanger
HEAT EXCHANGER↗
Acoustic prediction methods for rocket engines, including the effects of clustered engines and deflected exhaust flow
Acoustic prediction methods for rocket engines
ROCKET ENGINE↗
A program of X-ray astronomy from sounding rocket Final report
X-ray astronomy from sounding rockets
X-RAY ASTRONOMY↗
Design of rockets for maximum payload energy.
Analytical solution to determine rocket design for maximum payload energy
ROCKET ENGINE DESIGN↗
Flow system startup of a full-scale simulated nuclear rocket engine.
Liquid hydrogen flow system startup of full scale simulated nuclear rocket engine
PROPELLANT TESTING↗
Radio propagation effects of rocket exhaust plasmas.
Rocket exhaust plasma disturbance on radio transmission between vehicle and ground station noting multipath, forward and backscatter
PLASMA-ELECTROMAGNETIC INTERACTION↗
Optimization of step rockets by the discrete maximum principle.
Optimum stage weight distribution in multistage rocket obtained by discrete maximum principle
WEIGHT FACTOR↗
Rocket measurements of S sub q currents at midlatitude.
Midlatitude ionospheric currents detected by rocketborne rubidium vapor magnetometers in Nike- Apache rockets
IONOSPHERIC CURRENT↗
Base heating scaling criteria for a four- engine rocket cluster operating at high altitude.
Base heating scaling criteria for four-engine rocket cluster operating at high altitude
NOZZLE WALL↗
Radiative properties of carbon particles produced by a rocket motor.
Radiation from carbon particle clouds produced by research rocket motors
RADIATION MEASUREMENT↗
Rocket observations of the structure of the mesosphere.
Pressure, density, temperature and wind measurements in mesosphere resulted from rocket soundings to determine structure
MERIDIONAL FLOW↗
The unguided solid rocket for aerodynamic testing.
Operational problems and costs of staged solid- propellant rocket vehicles for atmosphere only, noting aerodynamic stabilization, spin motors, stage separation, jet plume, etc
ECONOMICS↗
Rocket measurements of cosmic-noise intensities below 5 Mc/s.
Cosmic radio-noise intensities below 5 mc measured by rocket probe
ROCKET SOUNDING↗
Data acquisition during static rocket testing.
Data acquisition of acoustic, vibration and heat flux during static rocket testing, using balloon rigging arrangement
SOUND MEASUREMENT↗