The previous 'Art of Injector Design' is maturing and merging with the more systematic 'Science of Combustion Device Analysis.' This technology can be based upon observation, correlation, experimentation and ultimately analytical modeling based upon basic engineering principles. This methodology is more systematic and far superior to the historical injector design process of 'Trial and Error' or blindly 'Copying Past Successes.' The benefit of such an approach is to be able to rank candidate design concepts for relative probability of success or technical risk in all the important combustion device design requirements and combustion process development risk categories before committing to an engine development program. Even if a single anal...
Operating characteristics and design aspects of injector, combustion chamber, and exhaust nozzle for...
Criteria for the design and development of turbines for rocket engines to meet specific performance,...
Characterization of liquid rocket engine injector elements is an important part of the development p...
NASA is developing the Space Launch System (SLS) for crewed exploration missions beyond low Earth or...
The performance and stability of liquid rocket engines is determined to a large degree by atomizatio...
Injector design criteria are provided for gaseous hydrogen-gaseous oxygen propellants. Design equati...
The turbopump system, from preliminary design through rocket engine testing is examined. Selection o...
Injector design guidelines are provided for gas/liquid propellant systems. Information was obtained ...
Subscale and full scale test firings of M-1 injector to improve combustion efficienc
Liquid propellant rocket engine conference proceedings and parameters for design of rocket engines a...
The choice of tools used for injector design is in a transitional phase between exclusive reliance o...
The overall structure and capabilities of an expert system designed to evaluate rocket engine perfor...
Statistical correlation between engine design and combustion stability in liquid propellant rocket e...
Control over drop size distributions, injection rates, and geometrical distribution of fuel and oxid...
Control over drop size distributions, injection rates, and geometrical distribution of fuel and oxid...
Operating characteristics and design aspects of injector, combustion chamber, and exhaust nozzle for...
Criteria for the design and development of turbines for rocket engines to meet specific performance,...
Characterization of liquid rocket engine injector elements is an important part of the development p...
NASA is developing the Space Launch System (SLS) for crewed exploration missions beyond low Earth or...
The performance and stability of liquid rocket engines is determined to a large degree by atomizatio...
Injector design criteria are provided for gaseous hydrogen-gaseous oxygen propellants. Design equati...
The turbopump system, from preliminary design through rocket engine testing is examined. Selection o...
Injector design guidelines are provided for gas/liquid propellant systems. Information was obtained ...
Subscale and full scale test firings of M-1 injector to improve combustion efficienc
Liquid propellant rocket engine conference proceedings and parameters for design of rocket engines a...
The choice of tools used for injector design is in a transitional phase between exclusive reliance o...
The overall structure and capabilities of an expert system designed to evaluate rocket engine perfor...
Statistical correlation between engine design and combustion stability in liquid propellant rocket e...
Control over drop size distributions, injection rates, and geometrical distribution of fuel and oxid...
Control over drop size distributions, injection rates, and geometrical distribution of fuel and oxid...
Operating characteristics and design aspects of injector, combustion chamber, and exhaust nozzle for...
Criteria for the design and development of turbines for rocket engines to meet specific performance,...
Characterization of liquid rocket engine injector elements is an important part of the development p...