Add to ORKGPhotographs, thermocouples, and emission spectra used to study mixing and reaction of hydrazine and nitrogen tetroxid
The potentials of using hydrazine as an alternative source of energy was studied. Three chemical rea...
Dynamic stability and performance of injectors, rocket liners, and supersonic combustor
Since the 1960s hydrazine (N2H4) is the commonly used monopropellant for various space propulsion sy...
Measuring heat and gas release rates for initial reaction of liquid nitrogen tetroxide with hydrazin...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
Chemical analysis, physical properties, and combustion characteristics of hydrazine nitrat
Measurement of heat release rate for liquid phase reaction of nitrogen tetroxide and hydrazin
Infrared spectroscopic analysis of combustion products released by nitrogen tetroxide disposal uni
Gaseous reactant combustion simulation of dimethylhydrazine and hydrazine fuel system for nonequilib...
To monitor hydrazine concentrations accurately and safely, hydrazine is converted into a stable deri...
Mechanism and design parameter effects in stream mixing and separation of nitrogen tetroxide-hydrazi...
Injector-element physical size effect on mixing and combustion of nitrogen tetroxide-hydrazine prope...
Effects of radiation on stability and compatibility of hydrazine and hydrazine-24 percent hydrazine ...
The initial rates of heat release produced by the reactions of hydrazine and unsymmetrical dimethylh...
The propulsion of most of the operating satellites comprises monopropellant (hydrazine - N2H4) or bi...
The potentials of using hydrazine as an alternative source of energy was studied. Three chemical rea...
Dynamic stability and performance of injectors, rocket liners, and supersonic combustor
Since the 1960s hydrazine (N2H4) is the commonly used monopropellant for various space propulsion sy...
Measuring heat and gas release rates for initial reaction of liquid nitrogen tetroxide with hydrazin...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
Chemical analysis, physical properties, and combustion characteristics of hydrazine nitrat
Measurement of heat release rate for liquid phase reaction of nitrogen tetroxide and hydrazin
Infrared spectroscopic analysis of combustion products released by nitrogen tetroxide disposal uni
Gaseous reactant combustion simulation of dimethylhydrazine and hydrazine fuel system for nonequilib...
To monitor hydrazine concentrations accurately and safely, hydrazine is converted into a stable deri...
Mechanism and design parameter effects in stream mixing and separation of nitrogen tetroxide-hydrazi...
Injector-element physical size effect on mixing and combustion of nitrogen tetroxide-hydrazine prope...
Effects of radiation on stability and compatibility of hydrazine and hydrazine-24 percent hydrazine ...
The initial rates of heat release produced by the reactions of hydrazine and unsymmetrical dimethylh...
The propulsion of most of the operating satellites comprises monopropellant (hydrazine - N2H4) or bi...
The potentials of using hydrazine as an alternative source of energy was studied. Three chemical rea...
Dynamic stability and performance of injectors, rocket liners, and supersonic combustor
Since the 1960s hydrazine (N2H4) is the commonly used monopropellant for various space propulsion sy...