Add to ORKGTwo alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
Ignition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen p...
Experimental performance of hydrogen-fluorine rocket engine at several chamber pressures and exhaust...
A preliminary analysis of the use of rocket-powered ejectors for pumping liquid oxygen and liquid hy...
Two hydrogen oxygen rocket engine system concepts were analyzed parametrically over a thrust range f...
Characteristic velocities of six single-element injectors that separately varied propellant spreadin...
This program demonstrated the feasibility of virtually all the components in present-day, high-energ...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
Technology for long life, high performing, gaseous hydrogen-gaseous oxygen rocket engines suitable f...
A survey is provided of hydrogen/oxygen (H/O) auxiliary propulsion system (APS) concepts and low thr...
Successful operation of a pulsing liquid hydrogen/liquid oxygen attitude control propulsion system t...
Chamber pressure variations and rocket combustor performance for gaseous hydrogen-liquid oxygen prop...
Preliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were use...
Ejectors (jet pumps, jet devices) are widely used in various branches of engineering. They are used...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
Ignition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen p...
Experimental performance of hydrogen-fluorine rocket engine at several chamber pressures and exhaust...
A preliminary analysis of the use of rocket-powered ejectors for pumping liquid oxygen and liquid hy...
Two hydrogen oxygen rocket engine system concepts were analyzed parametrically over a thrust range f...
Characteristic velocities of six single-element injectors that separately varied propellant spreadin...
This program demonstrated the feasibility of virtually all the components in present-day, high-energ...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
Technology for long life, high performing, gaseous hydrogen-gaseous oxygen rocket engines suitable f...
A survey is provided of hydrogen/oxygen (H/O) auxiliary propulsion system (APS) concepts and low thr...
Successful operation of a pulsing liquid hydrogen/liquid oxygen attitude control propulsion system t...
Chamber pressure variations and rocket combustor performance for gaseous hydrogen-liquid oxygen prop...
Preliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were use...
Ejectors (jet pumps, jet devices) are widely used in various branches of engineering. They are used...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
Ignition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen p...
Experimental performance of hydrogen-fluorine rocket engine at several chamber pressures and exhaust...