Feasibility study for a 44-inch first stage rocket motor Final report
Dynamic structure and stress analysis of Scout launch vehicle with 44 inch ALGOL engine
Source record↗
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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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Nonlinear combustion instability in liquid propellant rocket motors
Fluid dynamic model and diffusion-controlled flame analysis data on nonlinear combustion instability in liquid propellant rocket engines
Burstein, S. Z.↗
Design, fabrication, and testing of the applications technology satellite apogee motor chamber
Design, fabrication, and environmental testing of applications technology satellite apogee engine chamber
Kohorst, D. P.↗
Stress analysis of solid propellant rocket motors
Linear viscoelastic and elastic problem in stress analysis of solid propellant rocket engines
Akyuz, F. A.↗
Recent Measurements at JPL of Particle Size of Aluminum Oxide from Small Rocket Motors
Small rocket engine test firings conducted to measure particle size distribution of aluminum oxide exhausts
Dobbins, R. A.↗
Effect of instability during rotation on physiologic and perceptual-motor function Final report
Sinusoidal motion effects on crew performance during space flight
Source record↗
Nonlinear combustion instability in liquid propellant rocket motors
Mathematical models and computer program on nonlinear combustion instability in liquid propellant rocket engines
Burstein, S. Z.↗
Spin acceleration effects on some full-scale rocket motors.
Ballistic propellant combustion alteration and thermal effects due to dynamic spinning observed on solid propellant sounding rockets
Lucy, M. H.↗
Applied research and feasibility studies, experimental investigations and conceptual or preliminary design engineering applicable to inverters for motors program quarterly progress report, period ending dec. 25, 1967
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Irvine, D. B.↗
Lubrication of dc motors, slip rings, bearings, and gears for long-life space applications
Low vapor pressure lubrication for electrical and mechanical systems of OSO program
Mayer, R. W.↗
Scout standard 5th stage BE-3-A9 rocket motor propulsion unit program Final report
Modified BE-3 engine for fifth stage of Scout launch vehicle
Robertson, D. R.↗
Development of a thermal barrier coating for use on a water-cooled nozzle of a solid propellant rocket motor Final report
Thermal barrier coating for use on water cooled nozzle of solid propellant rocket engine
Stubbs, V. R.↗
Development of a filament wound case design for solid propellant rocket motors in the 260-inch diameter class Final report
Research and development of fiber glass filament wound engine case design for 260 inch diameter class solid propellant rocket engines
Vogt, C. W.↗
A comparison of experimental heat-transfer coefficients in a nozzle with analytical predictions from Bartz's methods for various combustion chamber pressures in a solid propellant rocket motor
Comparison of experimental heat transfer coefficients in a nozzle with analytical predictions for various combustion chamber pressures in solid rocket propellant engine
Smith, D. M.↗
A comparison of two methods of measuring particle size of Al sub 2 O sub 3 produced by a small rocket motor.
Tank collection and spectrophotometric tests in determining aluminum oxide particle size produced by small rocket engine
Dobbins, R. A.↗
General test plan for high energy upper stage motor static firing at Eniwetok Atoll
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R L Anderson↗
Motor brush wear measured with strain gages
Balanced bridge circuit, supplied with low-voltage direct current and connected to a readout device, measures remaining brush material, rate of brush wear, armature runout, and brush signature.
Farrell, W. T.↗