Add to ORKGA fuel performance database of liquid hydrocarbons and aluminum-hydrocarbon fuels was compiled using engine parametrics from the Space Transportation Engine Program as a baseline. Propellant performance parameters are introduced. General hydrocarbon fuel performance trends are discussed with respect to hydrogen-to-carbon ratio and heat of formation. Aluminum-hydrocarbon fuel performance is discussed with respect to aluminum metal loading. Hydrocarbon and aluminum-hydrocarbon fuel performance is presented with respect to fuel density, specific impulse, and propellant density specific impulse
Theoretical values of performance parameters for liquid hydrogen and liquid fluorine as a rocket pro...
Rocket propellant and propulsion technology improvements can reduce the development time and operati...
Two of the programs at the NASA Lewis Research Center investigating advanced systems for future spac...
The feasibility of using a heavy hydrocarbon fuel as a rocket propellant is examined. A method of pr...
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit July 10-13, 2005, Tucson, AZ.There ...
High pressure liquid rocket engine design, performance, weight, envelope, and operational characteri...
The application is studied of metallic H2 as a rocket propellant, which contains a specific energy o...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
A high pressure fuel coking testing apparatus was designed and developed and was used to evaluate th...
57th International Astronautical Congress October 2006, Valencia, Spain.A technique for determining...
An experimental program was conducted to study deposit formation in hydrocarbon fuels under flow con...
An experimental program was conducted to study deposit formation in hydrocarbon fuels under flow con...
This was a small-scale, hot-fire test series to make initial measurements of performance differences...
Hydrogen is the fuel of choice for hypersonic vehicles. Its main disadvantage is its low liquid and ...
An evaluation liquid oxygen (LOX) and various hydrocarbon fuels as low cost alternative propellants ...
Theoretical values of performance parameters for liquid hydrogen and liquid fluorine as a rocket pro...
Rocket propellant and propulsion technology improvements can reduce the development time and operati...
Two of the programs at the NASA Lewis Research Center investigating advanced systems for future spac...
The feasibility of using a heavy hydrocarbon fuel as a rocket propellant is examined. A method of pr...
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit July 10-13, 2005, Tucson, AZ.There ...
High pressure liquid rocket engine design, performance, weight, envelope, and operational characteri...
The application is studied of metallic H2 as a rocket propellant, which contains a specific energy o...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
A high pressure fuel coking testing apparatus was designed and developed and was used to evaluate th...
57th International Astronautical Congress October 2006, Valencia, Spain.A technique for determining...
An experimental program was conducted to study deposit formation in hydrocarbon fuels under flow con...
An experimental program was conducted to study deposit formation in hydrocarbon fuels under flow con...
This was a small-scale, hot-fire test series to make initial measurements of performance differences...
Hydrogen is the fuel of choice for hypersonic vehicles. Its main disadvantage is its low liquid and ...
An evaluation liquid oxygen (LOX) and various hydrocarbon fuels as low cost alternative propellants ...
Theoretical values of performance parameters for liquid hydrogen and liquid fluorine as a rocket pro...
Rocket propellant and propulsion technology improvements can reduce the development time and operati...
Two of the programs at the NASA Lewis Research Center investigating advanced systems for future spac...