Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
Gas pressurized, liquid bipropellant injection feed system starting flow transient criteria - effect...
Injection process influence on operating behavior of small liquid rockets - Hydrodynamic variables i...
Thrust augmentation in rocket engines using secondary injection in the diverging part of a nozzle is...
Single stage to orbit propulsion devices are being developed as part of low cost access to space end...
Gaseous nitrogen and argon were injected into a primary stream of air moving at Mach 2.56. The gase...
Secondary injection concept eliminates asymmetric loads and may increase thrust rocket engine loads ...
The flow field around the injection port for secondary injection of a gas normal to a supersonic str...
The How field around the injection port for secondary injection of a gas nor:mal to a super-sonic st...
Analytical investigation of side jet supersonic stream interaction including vortex flow in rocket n...
An experimental investigation, as part of a research program on the development of technology for th...
Flow interference caused by secondary injection in adverse pressure gradient nozzles - boundary laye...
This thesis explores the application of secondary injection thrust vector control (SITVC) to spacecr...
An analytical study was conducted to assess and estimate the level of effectiveness of an ejector/ro...
During a rocket launch, the point at which the most thrust is needed is at lift-off where the rocket...
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
Gas pressurized, liquid bipropellant injection feed system starting flow transient criteria - effect...
Injection process influence on operating behavior of small liquid rockets - Hydrodynamic variables i...
Thrust augmentation in rocket engines using secondary injection in the diverging part of a nozzle is...
Single stage to orbit propulsion devices are being developed as part of low cost access to space end...
Gaseous nitrogen and argon were injected into a primary stream of air moving at Mach 2.56. The gase...
Secondary injection concept eliminates asymmetric loads and may increase thrust rocket engine loads ...
The flow field around the injection port for secondary injection of a gas normal to a supersonic str...
The How field around the injection port for secondary injection of a gas nor:mal to a super-sonic st...
Analytical investigation of side jet supersonic stream interaction including vortex flow in rocket n...
An experimental investigation, as part of a research program on the development of technology for th...
Flow interference caused by secondary injection in adverse pressure gradient nozzles - boundary laye...
This thesis explores the application of secondary injection thrust vector control (SITVC) to spacecr...
An analytical study was conducted to assess and estimate the level of effectiveness of an ejector/ro...
During a rocket launch, the point at which the most thrust is needed is at lift-off where the rocket...
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
Gas pressurized, liquid bipropellant injection feed system starting flow transient criteria - effect...
Injection process influence on operating behavior of small liquid rockets - Hydrodynamic variables i...