Regenerative cooling capabilities of light hydrocarbon fuels when used with fluorinated oxidizer
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Hot firing tests with FLOX/methane propellants for evaluating pyrolytic refractory composite materia...
Testing thermal barrier coatings for flame surface of regeneratively cooled chamber operating with F...
Regenerative cooling capabilities of light hydrocarbon fuels used with FLOX and oxygen fluoride
Analysis to determine regenerative cooling limits of light hydrocarbons used with FLOX and OF2 over ...
Ceramic thermal protective coating system for regeneratively cooled hydrogen oxygen thrust chambe
To protect rocket metal surfaces from engine exhaust heat, a refractory thermal insulation mixture, ...
Program evaluates influences of heat transfer, stress, and cycle life. Coolant passages may be tubes...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
Insulating ceramic thermal barrier coatings can reduce gas turbine airfoil metal temperatures as muc...
The status of several coating programs is reviewed. These include efforts on protecting aircraft gas...
Fabrication and thermal performance of regeneratively cooled fluorine hydrogen thrust chambe
Protective coatings of refractory metals in rocket nozzles for liquid propellant
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Regenerative cooling capabilities of light hydrocarbon fuels when used with fluorinated oxidizer
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Hot firing tests with FLOX/methane propellants for evaluating pyrolytic refractory composite materia...
Testing thermal barrier coatings for flame surface of regeneratively cooled chamber operating with F...
Regenerative cooling capabilities of light hydrocarbon fuels used with FLOX and oxygen fluoride
Analysis to determine regenerative cooling limits of light hydrocarbons used with FLOX and OF2 over ...
Ceramic thermal protective coating system for regeneratively cooled hydrogen oxygen thrust chambe
To protect rocket metal surfaces from engine exhaust heat, a refractory thermal insulation mixture, ...
Program evaluates influences of heat transfer, stress, and cycle life. Coolant passages may be tubes...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
Insulating ceramic thermal barrier coatings can reduce gas turbine airfoil metal temperatures as muc...
The status of several coating programs is reviewed. These include efforts on protecting aircraft gas...
Fabrication and thermal performance of regeneratively cooled fluorine hydrogen thrust chambe
Protective coatings of refractory metals in rocket nozzles for liquid propellant
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Regenerative cooling capabilities of light hydrocarbon fuels when used with fluorinated oxidizer
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Hot firing tests with FLOX/methane propellants for evaluating pyrolytic refractory composite materia...