Status of the 260-inch diameter solid rocket motor program
Development of 260-inch diameter solid propellant rocket motor
Engineering topics
Publications and source records attributed to Ciepluch, C. C..
Development of 260-inch diameter solid propellant rocket motor
Method for igniting solid propellant rocket motors by injecting hypergolic fluids
Solid propellant ignition with hypergolic fluid injected to predetermined portions of propellant
Effect of composition on combustion of solid propellants during a rapid pressure drop
Performance of composite solid propellant at simulated high altitudes
Combustion efficiency of hydrogen fuel for varying afterburner configurations
Effect of variation of combustion chamber length and inlet temperature on low pressure-loss sea level afterburner
Low-pressure-loss short afterburner design for sea level thrust augmentation of axial flow turbojet engine