Add to ORKGGaseous reactant combustion simulation of dimethylhydrazine and hydrazine fuel system for nonequilibrium expansion studie
Flame propagation in supersonic premixed flows of hydrogen and air ignited by coaxial, hot gas, pilo...
Ignition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen p...
Engine performance and kinetic flow performance in nozzles using four space storable propellant comb...
Gaseous reactant combustion simulation of dimethylhydrazine and hydrazine fuel system for nonequilib...
Computer program for calculating inviscid one- dimensional nonequilibrium nozzle expansion of propel...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
Measuring heat and gas release rates for initial reaction of liquid nitrogen tetroxide with hydrazin...
Computer program calculates the inviscid one-dimensional equilibrium, frozen, and nonequilibrium noz...
Chamber technology for space storable propellant combinations featuring oxygen difluorid
Thrust losses due to the inability of dissociated combustion gases to recombine in exhaust nozzles a...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
Photographs, thermocouples, and emission spectra used to study mixing and reaction of hydrazine and ...
Chemical species and reactions of propellant systems determined for nonequilibrium flow - Performanc...
Computer program for calculating inviscid one-dimensional equilibrium, frozen and nonequilibrium noz...
Calculating equilibrium and kinetically limited performance using one dimensional mode
Flame propagation in supersonic premixed flows of hydrogen and air ignited by coaxial, hot gas, pilo...
Ignition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen p...
Engine performance and kinetic flow performance in nozzles using four space storable propellant comb...
Gaseous reactant combustion simulation of dimethylhydrazine and hydrazine fuel system for nonequilib...
Computer program for calculating inviscid one- dimensional nonequilibrium nozzle expansion of propel...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
Measuring heat and gas release rates for initial reaction of liquid nitrogen tetroxide with hydrazin...
Computer program calculates the inviscid one-dimensional equilibrium, frozen, and nonequilibrium noz...
Chamber technology for space storable propellant combinations featuring oxygen difluorid
Thrust losses due to the inability of dissociated combustion gases to recombine in exhaust nozzles a...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
Photographs, thermocouples, and emission spectra used to study mixing and reaction of hydrazine and ...
Chemical species and reactions of propellant systems determined for nonequilibrium flow - Performanc...
Computer program for calculating inviscid one-dimensional equilibrium, frozen and nonequilibrium noz...
Calculating equilibrium and kinetically limited performance using one dimensional mode
Flame propagation in supersonic premixed flows of hydrogen and air ignited by coaxial, hot gas, pilo...
Ignition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen p...
Engine performance and kinetic flow performance in nozzles using four space storable propellant comb...