SBIR-STTR Award

Silicon Carbide Microsensor with Piezoresistive Diamond Sensing Elements
Award last edited on: 4/10/2014

Sponsored Program
SBIR
Awarding Agency
DOD : MDA
Total Award Amount
$546,767
Award Phase
2
Solicitation Topic Code
SDIO92-014
Principal Investigator
Anthony D Kurtz

Company Information

Kulite Semiconductor Products Inc

One Willow Tree Road
Leonia, NJ 07605
   (201) 461-0900
   solomon@kulite.com
   www.kulite.com
Location: Multiple
Congr. District: 05
County: Bergen

Phase I

Contract Number: DAAL03-92-C-0043
Start Date: 7/1/1992    Completed: 1/1/1993
Phase I year
1992
Phase I Amount
$49,660
Currently, there exist no pressure sensors which are able to withstand operating temperatures in excess of 500 degrees Celsius. Such pressure measurements are critical for proper control of operating parameters in aeronautical propulsion systems, rockets and materials processing. Silicon pressure transducers, which have found extensive use in the aerospace industry, are inoperative above 600 degrees Celsius due to the unstable mechanical properties of silicon at those temperatures, and are unable to monitor pressure in the hot sections of aircraft engines. We, at Kulite, have initiated a program to develop ultra-high temperature pressure transducers using high temperature semiconductors, namely SiC and Diamond, as sensing elements. The program involves characterization of the materials, development of processing methods and most importantly, the demonstration of a prototype sensor capable of operation at temperatures up to 800 degrees Celsius. These transducers will revolutionize aerospace measurement capability by facilitating proper engine monitoring, enhanced fuel efficiency, and safety.

Phase II

Contract Number: DAAH04-94-C-0009
Start Date: 6/1/1994    Completed: 6/1/1996
Phase II year
1994
Phase II Amount
$497,107
Currently, there exist no pressure sensors which are able to withstand operating temperatures in excess of 500 degrees Celsius. Such pressure measurements are critical for proper control of operating parameters in aeronautical propulsion systems, rockets and materials processing. Silicon pressure transducers, which have found extensive use in the aerospace industry, are inoperative above 600 degrees Celsius due to the unstable mechanical properties of silicon at those temperatures, and are unable to monitor pressure in the hot sections of aircraft engines. We, at Kulite, have initiated a program to develop ultra-high temperature pressure transducers using high temperature semiconductors, namely SiC and Diamond, as sensing elements. The program involves characterization of the materials, development of processing methods and most importantly, the demonstration of a prototype sensor capable of operation at temperatures up to 800 degrees Celsius. These transducers will revolutionize aerospace measurement capability by facilitating proper engine monitoring, enhanced fuel efficiency, and safety.

Keywords:
PRESSURE SENSORS PROPULSION TRANSDUCERS SENSORS DIAMOND PROTOTYPE