The analysis, design, fabrication, and testing of a liquid rocket engine thrust chamber which is gas...
Analysis, design, fabrication, and test efforts were performed for the existing OF2/B2H6 regenerativ...
Chamber technology for space storable propellant combinations featuring oxygen difluorid
Analysis to determine regenerative cooling limits of light hydrocarbons used with FLOX and OF2 over ...
Regenerative cooling capabilities of light hydrocarbon fuels when used with fluorinated oxidizer
Thermal insulation development to reduce heat transfer to coolant of FLOX/propane regenerative engin
Program evaluates influences of heat transfer, stress, and cycle life. Coolant passages may be tubes...
The regenerative cooling limits (maximum chamber pressure) for 02/hydrocarbon gas generator and stag...
Testing thermal barrier coatings for flame surface of regeneratively cooled chamber operating with F...
Analytical and experimental study of regenerative cooling for FLOX methane engine with bulk boiling ...
Cooling systems for liquid propellant rocket engines operating at high chamber pressure
Fabrication and thermal performance of regeneratively cooled fluorine hydrogen thrust chambe
Design concepts, based on use of graphite as a thermal barrier for regeneratively cooled FLOX-methan...
A series of tests were performed in the NASA Glenn Research Centers Heated Tube Facility to study th...
Reliquefier design and cycles studied to reduce boiloff in extraterrestrial cryogenic propellant sto...
The analysis, design, fabrication, and testing of a liquid rocket engine thrust chamber which is gas...
Analysis, design, fabrication, and test efforts were performed for the existing OF2/B2H6 regenerativ...
Chamber technology for space storable propellant combinations featuring oxygen difluorid
Analysis to determine regenerative cooling limits of light hydrocarbons used with FLOX and OF2 over ...
Regenerative cooling capabilities of light hydrocarbon fuels when used with fluorinated oxidizer
Thermal insulation development to reduce heat transfer to coolant of FLOX/propane regenerative engin
Program evaluates influences of heat transfer, stress, and cycle life. Coolant passages may be tubes...
The regenerative cooling limits (maximum chamber pressure) for 02/hydrocarbon gas generator and stag...
Testing thermal barrier coatings for flame surface of regeneratively cooled chamber operating with F...
Analytical and experimental study of regenerative cooling for FLOX methane engine with bulk boiling ...
Cooling systems for liquid propellant rocket engines operating at high chamber pressure
Fabrication and thermal performance of regeneratively cooled fluorine hydrogen thrust chambe
Design concepts, based on use of graphite as a thermal barrier for regeneratively cooled FLOX-methan...
A series of tests were performed in the NASA Glenn Research Centers Heated Tube Facility to study th...
Reliquefier design and cycles studied to reduce boiloff in extraterrestrial cryogenic propellant sto...
The analysis, design, fabrication, and testing of a liquid rocket engine thrust chamber which is gas...
Analysis, design, fabrication, and test efforts were performed for the existing OF2/B2H6 regenerativ...
Chamber technology for space storable propellant combinations featuring oxygen difluorid