1. Vacuum plasma coatings for tubine blades;Holmes;Advanced High Pressure O2/H2 Technology, NASA CP 2372,1985
2. Durability of thermal barrier coatings in a high heat flux environment;Brindley;Advanced Earth-To-Orbit Propulsion Technology 1988, NASA CP 3012,1988
3. Heat transfer to throat tubes in a square-chambered rocket engine at NASA LeRC;Nesbitt;NASA TM 102336,1989
4. Vacuum application of thermal barrier plasma coatings;Holmes;Advanced Earth-to-Orbit Propulsion Technology 1988, NASA CP 3012,1988
5. Thermal modelling of various thermal barrier coatings in a high heat flux rocket engine;Nesbitt;NASA TM 102418,1989