Add to ORKGHigh Temperature issues in aircraft engines Hot section: Ni and Co based Superalloys Oxidation and Corrosion (Durability) at high temperatures. Thermal protection system (TPS) and RCC (Reinforced Carbon-Carbon) on the Space Shuttle Orbiter. High temperatures in other worlds: Planets close to their stars
High temperature materials research for hot section components of advanced air breathing jet engine
Thermal protection materials and systems (TPS) protect vehicles from the heat generated when enterin...
A wide range of programs are being conducted for improving the environmental resistance to oxidation...
Development of high temperature alloys, dispersion strengthened materials, composites, and coatings ...
NASA sponsored the Turbine Engine Hot Section Technology (HOST) Project to address the need for impr...
NASA sponsored the Turbine Engine Hot Section (HOST) project to address the need for improved durabi...
Interest in thermal protection systems for high-speed vehicles is increasing because of the stringen...
The topics addressed are: (1) Space Exploration Initiative (SEI); (2) Aeroassist Flight Experiment (...
The status of several coating programs is reviewed. These include efforts on protecting aircraft gas...
Aggressive fuel burn and carbon dioxide emission reduction goals for future gas turbine engines will...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
The Materials Division at the Lewis Research Center has a long record of contributions to both mater...
The objective of this work has been to develop more efficient, lighter weight, and higher temperatur...
A reinforced carbon-carbon thermal protection system is used on the space shuttle orbiter vehicle's ...
Research and plans concerning aircraft gas turbine engine hot section durability problems were discu...
High temperature materials research for hot section components of advanced air breathing jet engine
Thermal protection materials and systems (TPS) protect vehicles from the heat generated when enterin...
A wide range of programs are being conducted for improving the environmental resistance to oxidation...
Development of high temperature alloys, dispersion strengthened materials, composites, and coatings ...
NASA sponsored the Turbine Engine Hot Section Technology (HOST) Project to address the need for impr...
NASA sponsored the Turbine Engine Hot Section (HOST) project to address the need for improved durabi...
Interest in thermal protection systems for high-speed vehicles is increasing because of the stringen...
The topics addressed are: (1) Space Exploration Initiative (SEI); (2) Aeroassist Flight Experiment (...
The status of several coating programs is reviewed. These include efforts on protecting aircraft gas...
Aggressive fuel burn and carbon dioxide emission reduction goals for future gas turbine engines will...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
The Materials Division at the Lewis Research Center has a long record of contributions to both mater...
The objective of this work has been to develop more efficient, lighter weight, and higher temperatur...
A reinforced carbon-carbon thermal protection system is used on the space shuttle orbiter vehicle's ...
Research and plans concerning aircraft gas turbine engine hot section durability problems were discu...
High temperature materials research for hot section components of advanced air breathing jet engine
Thermal protection materials and systems (TPS) protect vehicles from the heat generated when enterin...
A wide range of programs are being conducted for improving the environmental resistance to oxidation...