The interior ballistics of the fluid controlled solid rocket motor
Fluid controlled solid rocket motor using fully oxidized solid propellant grain configured with oversized nozzle throat area
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Fluid controlled solid rocket motor using fully oxidized solid propellant grain configured with oversized nozzle throat area
Proportional hot gas secondary injection thrust vector control system for high energy solid propellant rocket motor
Radial acceleration spin effects on internal ballistics of rocket motor and combustion mechanism of solid propellant
Static test firing of 260 inch diameter solid rocket motors for demonstrating feasibility
Carbon phenolic, graphite phenolic, and silica phenolic nozzle ablative materials performance for large solid propellant rocket boosters
Applications Technology Satellite solid propellant apogee motor qualification tests
Flight subliming solid respin rocket system development for OV2-1 satellite and nozzle optimization performance studies
Thrust vector deflection angle requirements for controlling solid propellant launch vehicle
Subliming solid propellant attitude control rocket
Meteoroid hazards to solid propellant rocket motors
Development of 260-inch diameter solid propellant rocket motor
Scale model compressed air tests of 260-inch solid rocket with submerged nozzle to determine exhaust flow velocity and direction in annular channel
Feasibility, parametric design, and comparative analysis of unguided solid fuel rocket vehicle with solar orbit, earth probe, and reentry mission capabilities
Multiple start-stop solid propellant rocket motor using highly aluminized ammonium perchlorate annular propellant grains
Theoretical analysis of heat transfer in solid propellant rocket exhaust plumes by use of temperature probe located in plume environment
Auxiliary solid propellant motors in Saturn launch vehicle
Solid booster thrust decay control for payload or upper stage separation, noting inert slivers with auxiliary retrorockets as separation control
Effect on protective coatings of launch pads of exhaust products, chamber pressure, nozzle diameter, etc, from aluminized solid propellant rocket motors