Measuring heat and gas release rates for initial reaction of liquid nitrogen tetroxide with hydrazine, monomethyl hydrazine, and unsymmetric dimethyl hydrazin
Comparison, at simulated altitude, of nitrogen tetroxide/monomethylhydrazine and hydrogen peroxide/m...
The propulsion of most of the operating satellites comprises monopropellant (hydrazine - N2H4) or bi...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
Measurement of heat release rate for liquid phase reaction of nitrogen tetroxide and hydrazin
The initial rates of heat release produced by the reactions of hydrazine and unsymmetrical dimethylh...
Traditional hypergolic propellant combinations, such as those used on the space shuttle orbital mane...
Hypergolic systems rely on fuel and oxidizer propellant combinations that spontaneously ignite upon ...
Photographs, thermocouples, and emission spectra used to study mixing and reaction of hydrazine and ...
Gaseous reactant combustion simulation of dimethylhydrazine and hydrazine fuel system for nonequilib...
The combustion characteristics of hypergolic propellants are described. A research project was condu...
A two-part study was undertaken to investigate ignition of hypergolic propellants. The first part fo...
Chemical analysis, physical properties, and combustion characteristics of hydrazine nitrat
To monitor hydrazine concentrations accurately and safely, hydrazine is converted into a stable deri...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
Comparison, at simulated altitude, of nitrogen tetroxide/monomethylhydrazine and hydrogen peroxide/m...
The propulsion of most of the operating satellites comprises monopropellant (hydrazine - N2H4) or bi...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
Measurement of heat release rate for liquid phase reaction of nitrogen tetroxide and hydrazin
The initial rates of heat release produced by the reactions of hydrazine and unsymmetrical dimethylh...
Traditional hypergolic propellant combinations, such as those used on the space shuttle orbital mane...
Hypergolic systems rely on fuel and oxidizer propellant combinations that spontaneously ignite upon ...
Photographs, thermocouples, and emission spectra used to study mixing and reaction of hydrazine and ...
Gaseous reactant combustion simulation of dimethylhydrazine and hydrazine fuel system for nonequilib...
The combustion characteristics of hypergolic propellants are described. A research project was condu...
A two-part study was undertaken to investigate ignition of hypergolic propellants. The first part fo...
Chemical analysis, physical properties, and combustion characteristics of hydrazine nitrat
To monitor hydrazine concentrations accurately and safely, hydrazine is converted into a stable deri...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
Comparison, at simulated altitude, of nitrogen tetroxide/monomethylhydrazine and hydrogen peroxide/m...
The propulsion of most of the operating satellites comprises monopropellant (hydrazine - N2H4) or bi...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...