Add to ORKGEngine performance and kinetic flow performance in nozzles using four space storable propellant comb...
The objective of the presented work was to develop validated computational fluid dynamics (CFD) base...
Computerized simulation of high frequency instability in gas in liquid propellant rocket engine
Boundary flow composition in rocket motor combustion chamber with exhaust system samplin
Calculations of rocket and air breathing propulsion system combustion chamber and nozzle flow perfor...
Mixer design and experimental tank study for cryogenic propellants, with applications for manned Mar...
This report includes copies of relevant publications, including conference proceedings, resulting fr...
Detonability of gaseous hydrogen-oxygen mixtures under selected environmental condition
Combustor test results of the NASA Aerothermodynamic Integration Model are presented of a ramjet eng...
An experimental aerodynamic investigation was conducted to provide data for studies to determine the...
Comparison, at simulated altitude, of nitrogen tetroxide/monomethylhydrazine and hydrogen peroxide/m...
Chamber technology for space storable propellant combinations featuring oxygen difluorid
A chemical analysis of the emission and absorption spectra in the combustion chamber of a nitrogen t...
An analytical and experimental investigation was conducted to develop an understanding of the mechan...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Engine performance and kinetic flow performance in nozzles using four space storable propellant comb...
The objective of the presented work was to develop validated computational fluid dynamics (CFD) base...
Computerized simulation of high frequency instability in gas in liquid propellant rocket engine
Boundary flow composition in rocket motor combustion chamber with exhaust system samplin
Calculations of rocket and air breathing propulsion system combustion chamber and nozzle flow perfor...
Mixer design and experimental tank study for cryogenic propellants, with applications for manned Mar...
This report includes copies of relevant publications, including conference proceedings, resulting fr...
Detonability of gaseous hydrogen-oxygen mixtures under selected environmental condition
Combustor test results of the NASA Aerothermodynamic Integration Model are presented of a ramjet eng...
An experimental aerodynamic investigation was conducted to provide data for studies to determine the...
Comparison, at simulated altitude, of nitrogen tetroxide/monomethylhydrazine and hydrogen peroxide/m...
Chamber technology for space storable propellant combinations featuring oxygen difluorid
A chemical analysis of the emission and absorption spectra in the combustion chamber of a nitrogen t...
An analytical and experimental investigation was conducted to develop an understanding of the mechan...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Engine performance and kinetic flow performance in nozzles using four space storable propellant comb...
The objective of the presented work was to develop validated computational fluid dynamics (CFD) base...
Computerized simulation of high frequency instability in gas in liquid propellant rocket engine