The objective is to develop thin-film thermocouples for Space Shuttle Main Engine (SSME) components. Thin-film thermocouples have been developed for aircraft gas turbine engines and are in use for temperature measurement on turbine blades to 1800 F. The technology established for aircraft gas turbine engines will be adapted to the materials and environment encountered in the SSME. Specific goals are to expand the existing in-house thin-film sensor technology and to test the survivability and durability of thin-film sensors in the SSME environment
Parallel gap resistance welding was used to attach lead wires to sputtered thin film sensors. Ranges...
The use of thin films to electrically insulate thin film sensors on engine components minimizes the ...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
The objective is to develop thin film thermocouples (TFTC) for Space Shuttle Main Engine (SSME) comp...
As a demonstration of technology maturation, a thin-film temperature sensor probe was fabricated and...
Thin film thermocouples provide a minimally intrusive means of measuring surface temperature in host...
Thin film surface temperature sensors were developed. The sensors were made of platinum-platinum/10 ...
The Space Shuttle Main Engine (SSME) turbine environment stresses engine components to their design ...
Advanced thin film sensor techniques that can provide accurate surface strain and temperature measur...
Exploratory work is in progress to apply thin-film thermocouples to localized heat transfer measurem...
Prototype thin film heat flux sensors have been constructed and tested. The sensors can be applied t...
Advanced thin film sensors that can provide accurate surface temperature, strain, and heat flux meas...
The paper describes a proof-of-concept experiment on thin-film thermocouples used for localized heat...
The fabrication, materials characterization, and performance of thin film platinum rhodium thermocou...
The increasing trend towards high-temperature, fuel efficient jet engines has led to the development...
Parallel gap resistance welding was used to attach lead wires to sputtered thin film sensors. Ranges...
The use of thin films to electrically insulate thin film sensors on engine components minimizes the ...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
The objective is to develop thin film thermocouples (TFTC) for Space Shuttle Main Engine (SSME) comp...
As a demonstration of technology maturation, a thin-film temperature sensor probe was fabricated and...
Thin film thermocouples provide a minimally intrusive means of measuring surface temperature in host...
Thin film surface temperature sensors were developed. The sensors were made of platinum-platinum/10 ...
The Space Shuttle Main Engine (SSME) turbine environment stresses engine components to their design ...
Advanced thin film sensor techniques that can provide accurate surface strain and temperature measur...
Exploratory work is in progress to apply thin-film thermocouples to localized heat transfer measurem...
Prototype thin film heat flux sensors have been constructed and tested. The sensors can be applied t...
Advanced thin film sensors that can provide accurate surface temperature, strain, and heat flux meas...
The paper describes a proof-of-concept experiment on thin-film thermocouples used for localized heat...
The fabrication, materials characterization, and performance of thin film platinum rhodium thermocou...
The increasing trend towards high-temperature, fuel efficient jet engines has led to the development...
Parallel gap resistance welding was used to attach lead wires to sputtered thin film sensors. Ranges...
The use of thin films to electrically insulate thin film sensors on engine components minimizes the ...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
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