The Space Shuttle Main Engine (SSME) turbine environment stresses engine components to their design limits and beyond. The extremely high temperatures and rapid temperature cycling can easily cause parts to fail if they are not properly designed. Thin film heat flux sensors can provide heat loading information with almost no disturbance of gas flows or of the blade. These sensors can provide steady state and transient heat flux information. A thin film heat flux sensor is described which makes it easier to measure small temperature differences across very thin insulating layers
To monitor the high-intensity heat flux conditions that occur in the space shuttle main engine (SSME...
As a demonstration of technology maturation, a thin-film temperature sensor probe was fabricated and...
Tasks performed in this project were defined in a September 9, 1994 meeting of representatives of Va...
Prototype thin film heat flux sensors have been constructed and tested. The sensors can be applied t...
Thin Film Heat Flux Sensors: Design and Methodology: (1) Heat flux is one of a number of parameters,...
The objective is to develop thin-film thermocouples for Space Shuttle Main Engine (SSME) components....
A new thin-film heat flux gage has been fabricated specifically for severe high temperature operatio...
Thin film thermocouples provide a minimally intrusive means of measuring surface temperature in host...
Data reduction was completed for tests of plug-type heat flux sensors (gauges) in a turbine blade th...
The Heat Flux Microsensor is a new sensor which was recently patented by Virginia Tech and is just s...
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 objective is to develop thin film thermocouples (TFTC) for Space Shuttle Main Engine (SSME) comp...
Measurements of heat flux to space shuttle main engine (SSME) turbine blade surfaces are being made ...
There is a need to more thoroughly characterize the hostile space shuttle main engine (SSME) turbopu...
To monitor the high-intensity heat flux conditions that occur in the space shuttle main engine (SSME...
As a demonstration of technology maturation, a thin-film temperature sensor probe was fabricated and...
Tasks performed in this project were defined in a September 9, 1994 meeting of representatives of Va...
Prototype thin film heat flux sensors have been constructed and tested. The sensors can be applied t...
Thin Film Heat Flux Sensors: Design and Methodology: (1) Heat flux is one of a number of parameters,...
The objective is to develop thin-film thermocouples for Space Shuttle Main Engine (SSME) components....
A new thin-film heat flux gage has been fabricated specifically for severe high temperature operatio...
Thin film thermocouples provide a minimally intrusive means of measuring surface temperature in host...
Data reduction was completed for tests of plug-type heat flux sensors (gauges) in a turbine blade th...
The Heat Flux Microsensor is a new sensor which was recently patented by Virginia Tech and is just s...
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 objective is to develop thin film thermocouples (TFTC) for Space Shuttle Main Engine (SSME) comp...
Measurements of heat flux to space shuttle main engine (SSME) turbine blade surfaces are being made ...
There is a need to more thoroughly characterize the hostile space shuttle main engine (SSME) turbopu...
To monitor the high-intensity heat flux conditions that occur in the space shuttle main engine (SSME...
As a demonstration of technology maturation, a thin-film temperature sensor probe was fabricated and...
Tasks performed in this project were defined in a September 9, 1994 meeting of representatives of Va...