Add to ORKGSummary of industry survey and literature search of ignition spike phenomena in low thrust, hypergolic, liquid bipropellant rocket engine
Applicability of delta p approach to study of combustion instability in liquid and solid propellant ...
The effects of radiation on the performance of modern rocket propulsion systems operating at high pr...
Test program evaluates thermal and electric ignition mechanisms in selected nonmetallic materials fo...
Chemical analysis, physical properties, and combustion characteristics of hydrazine nitrat
Engine design and operating parameters studied for effects on rocket engine ignition and poppin
The combustion characteristics of hypergolic propellants are described. A research project was condu...
Effects of injector catalytic surfaces on ignition pressure spiking in Apollo command module engin
Comparison, at simulated altitude, of nitrogen tetroxide/monomethylhydrazine and hydrogen peroxide/m...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
A chemical analysis of the emission and absorption spectra in the combustion chamber of a nitrogen t...
Analytical model for describing combustion chamber disturbances during start transient and steady st...
The solution of problems of combustion instability for more effective communication between the vari...
The starting transients of solid propellant engines were investigated to develop design principles f...
A model is described which provides a means for analyzing the complexities of ignition transients an...
Experimental droplet burning rates obtained at atmospheric pressure in combustion gas environmen
Applicability of delta p approach to study of combustion instability in liquid and solid propellant ...
The effects of radiation on the performance of modern rocket propulsion systems operating at high pr...
Test program evaluates thermal and electric ignition mechanisms in selected nonmetallic materials fo...
Chemical analysis, physical properties, and combustion characteristics of hydrazine nitrat
Engine design and operating parameters studied for effects on rocket engine ignition and poppin
The combustion characteristics of hypergolic propellants are described. A research project was condu...
Effects of injector catalytic surfaces on ignition pressure spiking in Apollo command module engin
Comparison, at simulated altitude, of nitrogen tetroxide/monomethylhydrazine and hydrogen peroxide/m...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
A chemical analysis of the emission and absorption spectra in the combustion chamber of a nitrogen t...
Analytical model for describing combustion chamber disturbances during start transient and steady st...
The solution of problems of combustion instability for more effective communication between the vari...
The starting transients of solid propellant engines were investigated to develop design principles f...
A model is described which provides a means for analyzing the complexities of ignition transients an...
Experimental droplet burning rates obtained at atmospheric pressure in combustion gas environmen
Applicability of delta p approach to study of combustion instability in liquid and solid propellant ...
The effects of radiation on the performance of modern rocket propulsion systems operating at high pr...
Test program evaluates thermal and electric ignition mechanisms in selected nonmetallic materials fo...