Add to ORKGIgnition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen propellant mixture combustio
Data from prototype GO2-GH2 injection elements were obtained and analyzed. The bulk of the testing w...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
As a result of the need for a uniform hot gas test stream for fuel injector development for hydrogen...
The catalytic ignition of hydrogen and oxygen propellants was studied using a premixing hydrogen/oxy...
Quantitative values were computed which show the effects of the presence of small amounts of oxygen,...
An investigation of oxygen compatibility and resistance to ignition of candidate materials for use i...
Detonability of gaseous hydrogen-oxygen mixtures under selected environmental condition
Two hydrogen oxygen rocket engine system concepts were analyzed parametrically over a thrust range f...
Analysis, design, and demonstration of high performance injectors for liquid fluorine- gaseous hydro...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Vacuum test chamber to determine explosion and detonation hazards from venting of hydrogen and oxyge...
Inert gases, halogenated hydrocarbons for suppressing ignition of oxygen mixtures with hydrogen and ...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
Characteristic velocities of six single-element injectors that separately varied propellant spreadin...
Evaluation and demonstration of cryogenic propellant /oxygen-hydrogen/ use for spacecraft reaction c...
Data from prototype GO2-GH2 injection elements were obtained and analyzed. The bulk of the testing w...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
As a result of the need for a uniform hot gas test stream for fuel injector development for hydrogen...
The catalytic ignition of hydrogen and oxygen propellants was studied using a premixing hydrogen/oxy...
Quantitative values were computed which show the effects of the presence of small amounts of oxygen,...
An investigation of oxygen compatibility and resistance to ignition of candidate materials for use i...
Detonability of gaseous hydrogen-oxygen mixtures under selected environmental condition
Two hydrogen oxygen rocket engine system concepts were analyzed parametrically over a thrust range f...
Analysis, design, and demonstration of high performance injectors for liquid fluorine- gaseous hydro...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Vacuum test chamber to determine explosion and detonation hazards from venting of hydrogen and oxyge...
Inert gases, halogenated hydrocarbons for suppressing ignition of oxygen mixtures with hydrogen and ...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
Characteristic velocities of six single-element injectors that separately varied propellant spreadin...
Evaluation and demonstration of cryogenic propellant /oxygen-hydrogen/ use for spacecraft reaction c...
Data from prototype GO2-GH2 injection elements were obtained and analyzed. The bulk of the testing w...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
As a result of the need for a uniform hot gas test stream for fuel injector development for hydrogen...