The penetration of gaseous nitrogen into liquid oxygen at a pressure of 150 psi was determined by monitoring the composition of the evaporating liquid in a nitrogen analyzer. For pressurization times of about 1 hr the penetration depth varies between 0.0024 and 0.018 in. at an evaporation rate of about 1 gal/day. These are small compared to the penetration depth of 22.2 in. measured in the 7-inch high temperature tunnel at a pressure of 1500 psi, pressurization time of 5 min, and evaporation rate of 121 gal/day
Self pressurization by propellant boiloff is experimentally studied as an alternate pressurization c...
Introduction. - At moderately high pressures, the decomposition of gaseous nitrogen pentoxide was sh...
Liquid nitrogen or other cryogenic liquids have the potential to replace or augment current energy s...
In order to meet the need for propulsion testing in the high supersonic range from Mach 4 to Mach 7,...
Analytical model development for contamination study of liquid oxygen by gaseous nitroge
Depressurization of water containing various concentrations of dissolved nitrogen gas was studied. I...
The sound speed in liquid oxygen (LOX), liquid nitrogen (LN2), and five LOX-LN2 mixtures was measure...
Experimental measurements of critical flow rate and pressure ratio for nitrogen flowing through a no...
A cryogenic wind tunnel is based on the twofold idea of lowering drive power and increasing Reynolds...
This paper compares a fluid/thermal simulation, in Fluent, with a low-g, nitrogen slosh and boiling ...
A clean source of high enthalpy air was obtained from the exothermic decomposition of nitric oxide i...
The Liquid Nitrogen Test Facility is a unique test facility for ground-based liquid nitrogen experim...
Velocity-profile, pitot-pressure, and supplemental probe measurements were made at the nozzle exist ...
In the context of an overall development of transonic, cryogenic wnd tunnel technology, NASA has bee...
Choked flow rates and axial pressure distributions were measured for subcooled nitrogen in a converg...
Self pressurization by propellant boiloff is experimentally studied as an alternate pressurization c...
Introduction. - At moderately high pressures, the decomposition of gaseous nitrogen pentoxide was sh...
Liquid nitrogen or other cryogenic liquids have the potential to replace or augment current energy s...
In order to meet the need for propulsion testing in the high supersonic range from Mach 4 to Mach 7,...
Analytical model development for contamination study of liquid oxygen by gaseous nitroge
Depressurization of water containing various concentrations of dissolved nitrogen gas was studied. I...
The sound speed in liquid oxygen (LOX), liquid nitrogen (LN2), and five LOX-LN2 mixtures was measure...
Experimental measurements of critical flow rate and pressure ratio for nitrogen flowing through a no...
A cryogenic wind tunnel is based on the twofold idea of lowering drive power and increasing Reynolds...
This paper compares a fluid/thermal simulation, in Fluent, with a low-g, nitrogen slosh and boiling ...
A clean source of high enthalpy air was obtained from the exothermic decomposition of nitric oxide i...
The Liquid Nitrogen Test Facility is a unique test facility for ground-based liquid nitrogen experim...
Velocity-profile, pitot-pressure, and supplemental probe measurements were made at the nozzle exist ...
In the context of an overall development of transonic, cryogenic wnd tunnel technology, NASA has bee...
Choked flow rates and axial pressure distributions were measured for subcooled nitrogen in a converg...
Self pressurization by propellant boiloff is experimentally studied as an alternate pressurization c...
Introduction. - At moderately high pressures, the decomposition of gaseous nitrogen pentoxide was sh...
Liquid nitrogen or other cryogenic liquids have the potential to replace or augment current energy s...