Add to ORKGThermal barrier coating for use on water cooled nozzle of solid propellant rocket engin
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
Subscale rocket thrust chamber tests were conducted to evaluate the effectiveness and durability of ...
Ceramic thermal protective coating system for regeneratively cooled hydrogen oxygen thrust chambe
Testing thermal barrier coatings for flame surface of regeneratively cooled chamber operating with F...
Design and fabrication of shadow shield system for thermal protection of liquid hydrogen propellant ...
Protective coating of phosphate-bonded zirconia for regeneratively cooled thrust chamber
The invention is particularly concerned with sealing thermal barrier coating systems of the type in ...
NASA has played a central role in the development of thermal barrier coatings (TBCs) for gas turbine...
Testing polymeric coatings for use in space simulation chamber - resistance to abrasion, acids, ther...
Development of protective coating system for regeneratively cooled thrust chamber
Protective coatings of refractory metals in rocket nozzles for liquid propellant
Methods for applying thermal barrier coatings to the hot-gas side wall of rocket thrust chambers in ...
Protective coating systems for refractory metal used in rocket engine nozzles - rocket engine test f...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
Subscale rocket thrust chamber tests were conducted to evaluate the effectiveness and durability of ...
Ceramic thermal protective coating system for regeneratively cooled hydrogen oxygen thrust chambe
Testing thermal barrier coatings for flame surface of regeneratively cooled chamber operating with F...
Design and fabrication of shadow shield system for thermal protection of liquid hydrogen propellant ...
Protective coating of phosphate-bonded zirconia for regeneratively cooled thrust chamber
The invention is particularly concerned with sealing thermal barrier coating systems of the type in ...
NASA has played a central role in the development of thermal barrier coatings (TBCs) for gas turbine...
Testing polymeric coatings for use in space simulation chamber - resistance to abrasion, acids, ther...
Development of protective coating system for regeneratively cooled thrust chamber
Protective coatings of refractory metals in rocket nozzles for liquid propellant
Methods for applying thermal barrier coatings to the hot-gas side wall of rocket thrust chambers in ...
Protective coating systems for refractory metal used in rocket engine nozzles - rocket engine test f...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
Subscale rocket thrust chamber tests were conducted to evaluate the effectiveness and durability of ...