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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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Mass flow rate of gas evolution from burning solid rocket propellant during transient depressurization of combustion chamber
Solid propellant composition and rocket motor design effect on plasma microwave and visible light attenuation emitted by exhaust
Propellants for space flight reviewing rocket propulsion and Moon mission, emphasizing costs
Flox-light hydrocarbon combinations desirable as liquid rocket propellants due to high specific impulse, hypergolicity and cooling properties
Earth storable propellants exist in liquid phase in near-Earth temperatures at vapor pressure below 100 psi and hypergolic, yielding simple, reliable and predictable systems
Cryogenic weigh system for calibrating propellant masses for Saturn S-IV stage
Low pressure combustion of solid propellants noting extinction, aluminum concentration, oxidizer particle size, etc
Mechanical stress effects on permeability of engineering materials to cryogenic and storable launch vehicle propellants
Free-floating thin film liner for glass fiber cryogenic propellant tank
Flame spreading over surface of igniting composite solid propellant constituents
Pressurization gas requirements for cryogenic liquid propellant tanks
Fuel cells using storable rocket propellants for reactants
Theoretical studies of processes occurring during rapid depressurization of burning solid propellants
Dimensional analysis used to derive general equation for predicting gas pressurization requirements in cylindrical and spherical liquid propellant tanks
Proportional two-stage valve with closed loop pressure feedback logic for high temperature solid propellant pneumatic system
Annotated bibliography on low-g liquid propellant behavior
Mass flow rate of gas evolution from burning solid rocket propellant during transient depressurization of combustion chamber
Overpressure of liquid propellant explosion in vacuum and atmosphere