High-temperature environment operable sensors and electronics are required for exploring the inner solar planets and distributed control of next generation aeronautical engines. Various silicon carbide (SiC) high temperature sensors, actuators, and electronics have been demonstrated at and above 500C. A compatible packaging system is essential for long-term testing and application of high temperature electronics and sensors. High temperature passive components are also necessary for high temperature electronic systems. This talk will discuss ceramic packaging systems developed for high temperature electronics, and related testing results of SiC circuits at 500C and silicon-on-insulator (SOI) integrated circuits at temperatures beyond commer...
Electronic applications are described that would benefit from the availability of high temperature s...
A brief overview is presented of the sensors and electronics development work ongoing at NASA Glenn ...
The development of new aircraft engines requires the measurement of pressures in hot areas such as t...
High-temperature environment operable sensors and electronics are required for long-term exploration...
NASA space and aeronautical missions for probing the inner solar planets as well as for in situ moni...
This paper reviews ceramic substrates and thick-film metallization based packaging technologies in d...
High-temperature electronics and sensors are necessary for harsh-environment space and aeronautical ...
This paper reviews ceramic substrates and thick-film metallization based packaging technologies in d...
A ceramic- and thick-film-materials-based prototype electronic package designed for silicon carbide ...
Gold thick-film metallization and 96 alumina substrate based prototype packaging system developed fo...
A series of ceramic substrates and thick-film metalization-based prototype microsystem packages desi...
A high temperature co-fired ceramic (HTCC) alumina material was previously electrically tested at te...
To meet the needs of the aerospace propulsion and space power communities, the high temperature elec...
In recent years, the aerospace propulsion and space power communities have expressed a growing need ...
The semiconducting properties of electronic grade silicon carbide crystals, such as wide energy band...
Electronic applications are described that would benefit from the availability of high temperature s...
A brief overview is presented of the sensors and electronics development work ongoing at NASA Glenn ...
The development of new aircraft engines requires the measurement of pressures in hot areas such as t...
High-temperature environment operable sensors and electronics are required for long-term exploration...
NASA space and aeronautical missions for probing the inner solar planets as well as for in situ moni...
This paper reviews ceramic substrates and thick-film metallization based packaging technologies in d...
High-temperature electronics and sensors are necessary for harsh-environment space and aeronautical ...
This paper reviews ceramic substrates and thick-film metallization based packaging technologies in d...
A ceramic- and thick-film-materials-based prototype electronic package designed for silicon carbide ...
Gold thick-film metallization and 96 alumina substrate based prototype packaging system developed fo...
A series of ceramic substrates and thick-film metalization-based prototype microsystem packages desi...
A high temperature co-fired ceramic (HTCC) alumina material was previously electrically tested at te...
To meet the needs of the aerospace propulsion and space power communities, the high temperature elec...
In recent years, the aerospace propulsion and space power communities have expressed a growing need ...
The semiconducting properties of electronic grade silicon carbide crystals, such as wide energy band...
Electronic applications are described that would benefit from the availability of high temperature s...
A brief overview is presented of the sensors and electronics development work ongoing at NASA Glenn ...
The development of new aircraft engines requires the measurement of pressures in hot areas such as t...