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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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Experimental verification of double dead time model describing chugging in liquid bipropellant rocket engines
Concentric tube injection effect on dynamic characteristics of hydrogen-oxygen rocket
Nonlinear combustion instability in liquid propellant rocket engines, describing nonsteady combustion process with aid of Crocco time-lag hypothesis
Working equations for dimensions and orientation of impinging propellant sheets in liquid rocket engine injectors
Surveyor throttleable liquid propellant rocket engine for operation on propellants saturated with dissolved liquid gas
Effect on protective coatings of launch pads of exhaust products, chamber pressure, nozzle diameter, etc, from aluminized solid propellant rocket motors
Mechanical construction of two types of Gerdien condenser rocket probes, noting instrumentation racks and inflatable parachutes for descent
Micrometeoroid sampling with Luster sounding rocket during Leonid meteor shower, detailing contamination control program
Transient heat transfer and thermal stresses for nuclear rocket due to sudden hydrogen coolant flow increase
Ignition pressure transient in solid rocket motors, examining chamber filling interval, flame propagation, heat transfer correlation, burning area, etc
Spectral radiance of model rocket exhaust gases measured by rapid scanning spectrometer at simulated altitude
Air loads on sounding rocket from distributed aerodynamics and pressure differential
Error in application of WKB method to linearized postburnout equation of motion of sounding rocket
Ballistic propellant combustion alteration and thermal effects due to dynamic spinning observed on solid propellant sounding rockets
Liquid propellant utilization for sounding rockets
Balancing operations for rocket vehicles and payloads, defining terms, establishing relation between static and dynamic imbalance and flight vehicle motions, etc
Static and dynamic combustion phenomena effects on grain structural design for solid propellant rocket engine
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