Summary of a Study of the Low-pressure Combustion of Solid Propellants
Solid propellant low pressure instability and extinguishment
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Solid propellant low pressure instability and extinguishment
Solid propellants combustion characteristics under hypergolic fluid injection control conditions including burning rate, vacuum ignition, low pressure stability, etc
Solid propellants stress measurement using piezoresistive transducer
Saturated hydrocarbon polymeric binder for advanced solid propellant and hybrid solid grain
Glass transition temperature measurement - telomer preparation and reactions
Saturated hydrocarbon polymeric binder materials prepared for advanced solid propellant and hybrid solid grain
Saturated hydrocarbon polymeric binder for advanced solid propellant and hybrid solid grains
Saturated hydrocarbon polymeric binder for advanced solid propellant and hybrid solid grain
Saturated hydrocarbon polymeric binder for advanced solid propellant and hybrid solid grains
Saturated hydrocarbon polymeric binder for solid propellant and hybrid solid grain
Composite solid propellants surface structure and profile characteristics burning with various oxidizers and polyurethane binder by scanning electron microscopy
Saturated hydrocarbon polymeric binder for solid propellant and hybrid propellant grains
Solid propellant ignition and ignition propagation for rocket exhaust and hypergolic-type igniters
Solid propellant composition and rocket motor design effect on plasma microwave and visible light attenuation emitted by exhaust
Solid propellant engineering, binder curing reactions, ATS engine development, pintle nozzle thrust vector control, and low pressure combustion
Burning solid propellant behavior under pressure fluctuations expressed in response function terms defining small mass flux change ratio to small pressure change
Solid propellant ignition with hypergolic fluid injected to predetermined portions of propellant
Aluminized solid propellant transient burning rate augmentation during acceleration loads