Solid propellant rocket motor performance computer programs using the group transformation method
Solid propellant rocket engine performance computer programs using group transformation method
SOLID PROPELLANT ROCKET ENGINE↗
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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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Design, proof test and delivery program of TE-372-3 Pyrogen for TE-29 Recruit rocket motor Final report
Design modifications, proof test, and delivery program of igniters for Recruit rocket engines
IGNITION SYSTEM↗
Ignition and ignition propagation in solid propellant motors.
Solid propellant ignition and ignition propagation for rocket exhaust and hypergolic-type igniters
CHAMBER PRESSURE↗
Dc motors make a comeback in space
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Studer, P. A.↗
Design and development of the Castor IIA ROCKET motor Final report
Design, development, and qualification testing of Castor IIA rocket engine for second stage Scout launch vehicle application
ENGINE DESIGN↗
The effects of sensory deprivation on sensory, perceptual, motor, cognitive, and physiological functions
Sensory deprivation effects on human sensory, perceptual, and physiological mechanisms
VISUAL PERCEPTION↗
Study on the spectral emissivity of carbon particles produced by a rocket motor Final report
Spectral emissivity of carbon particles in exhaust gases of rocket engines using oxygen and RP-1 PROPELLANTS
SPECTRAL EMISSION↗
Performance of X 258 third-stage motor on Delta 36 /OT-3/
In-flight performance of solid propellant rocket engine for Delta launch vehicle
DELTA LAUNCH VEHICLE↗
Nonlinear aspects of combustion instability in liquid propellant rocket motors Status report, 1 Jun. 1966 - 31 May 1967
Nonlinear aspects of combustion instability in liquid propellant rocket engines
NONLINEARITY↗
A method for obtaining temperature profiles for solid propellant motor exhaust streams.
Theoretical analysis of heat transfer in solid propellant rocket exhaust plumes by use of temperature probe located in plume environment
SOLID PROPELLANT ROCKET ENGINE↗
Interrelations between combustion phenomena and mechanical properties in solid propellant rocket motors.
Static and dynamic combustion phenomena effects on grain structural design for solid propellant rocket engine
PROPELLANT GRAIN↗
The dynamics of solid propellant rocket motors.
Solid rocket engine propellant grain structural dynamics including elastic and viscoelastic deformations, stress and shear vibration modes, natural frequency calculations, etc, using Fourier inversions and transforms
VISCOELASTICITY↗
Status of the 260-inch diameter solid rocket motor program.
Third 260-inch diameter solid propellant rocket engine test firing
NOZZLE GEOMETRY↗
Ultra low voltage dc motor generator program, phase 1 Final report
Liquid metal collectors for spacecraft ultra low voltage power source
Ratti, N.↗
Nonlinear combustion instability in liquid-propellant rocket motors
Gas dynamic model for nonlinear combustion instability analysis in liquid propellant rocket engines
Burstein, S. Z.↗
Two hundred sixty SL-3 motor program Final report
Design, fabrication, and test firing of 260 inch diameter solid rocket engine
Source record↗
Thiokol 260-SL subscale nozzle verification program, 65-SS-2 and 65-SS-3 motors
Static tests of 65 inch diameter subscale rocket engines to evaluate nozzle fabrication methods, nozzle materials, liner material, case insulation, and propellant
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Experimental investigation of acoustic liners to suppress screech in storable propellant rocket motors
Experimental, and theoretical evaluations of acoustic liners for screech suppression in rocket engines
Phillips, B.↗