Acoustic losses of a subscale, cold-flow rocket motor for various ''J'' values
Geometric variables effect on acoustic attenuation in axial mode combustion instability in subscale rocket engine models
ACOUSTIC ATTENUATION↗
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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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Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. II - Overall two-stage performance
Cold flow test of pump drive turbines for M-1 rocket engine
M-1 ROCKET ENGINE↗
Particle size of aluminum oxide produced by a small rocket motor
Spectrophotometric method for measurement of aluminum oxide particle sizes during burning of solid propellant rocket engine
ALUMINUM OXIDE↗
Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies
Flight test of nose mounted rotating solid propellant rocket attitude control system for space vehicle second stage
ATTITUDE CONTROL↗
Effect of propellant injection velocity on screech in 20,000-pound hydrogen-oxygen rocket engine
Propellant injection velocity effect on screech in 20,000 pound hydrogen-oxygen rocket engine
ROCKET ENGINE↗
NASA Langley small meteorological sounding rocket development program
Small meteorological sounding rocket system development for upper atmosphere parameters
NASA PROGRAM↗
Evaluation of the Marc 7G1 auxiliary rocket motor for use on the Atlas-Centaur vehicle Final report
Evaluation of Mars 7G1 auxiliary rocket motor for use as retrograde thrust generator on Atlas-Centaur space vehicle
ATLAS CENTAUR LAUNCH VEHICLE↗
One-dimensional nonlinear model for determining combustion instability in solid propellant rocket motors
Nonlinear analysis of combustion instability in solid propellant rocket engines
SOLID PROPELLANT ROCKET ENGINE↗
Further studies of liquid sloshing in rocket propellant tanks Final report, 25 Mar. 1961 - 31 Dec. 1965
Liquid sloshing and dynamics in rocket propellant tanks annotated bibliography with abstracts
ABSTRACT↗
Density-altitude data from 150 rocket flights and 26 searchlight probings, 1947 through 1964
Density and altitude data from rocket flights and searchlight probings
ATMOSPHERIC DENSITY↗
Oscillatory combustion in rockets Third semiannual report, Jun. 1 - Nov. 30, 1965
Rocket engine oscillatory combustion studies
ROCKET ENGINE↗
Acoustic decay coefficients of simulated rocket combustors
Acoustic decay coefficients of simulated rocket combustors
ACOUSTICS↗
Rocket measurements of energetic electron precipitation in the auroral zone
Rocket measurements of energetic electron precipitation in auroral zone
ELECTRON PRECIPITATION↗
Performance of rocket nozzle materials with several solid propellants
Erosion resistance and thermal stress cracking tests of rocket nozzle materials with solid propellants
THERMAL STRESS↗
Tungsten nuclear rocket, phase I, part 1 Final report
Tungsten water moderated nuclear rocket reactor experiments and analyses
NUCLEAR ROCKET↗
Analytical and experimental study of ablation material for rocket engine application Final report
Techniques for rating performance of ablative materials in liquid-propellant rocket engines
ABLATING MATERIAL↗
A Theoretical Study of Nonlinear Transverse Combustion Instability in Liquid Propellant Rocket Motors
Nonsteady flow conditions in subsonic section of Laval nozzle to investigate nonlinear transverse combustion instability in liquid propellant rocket motors
COMBUSTION INSTABILITY↗
Experimental Auxiliary Rocket Engine, Part I Final Report
Design and development of rocket engine for spacecraft reaction control and maneuvering systems
REACTION CONTROL↗