SBIR/STTR Research Award
Thermal Pyrolytic Graphite (TPG) Embedded Copper Graphite Composite Heat Sinking Slat for Phase Array Radar Antenna
Award amount
$148,000Program and phase
SBIR · Phase IAward year
2005Award details
- Awarding agency
- Department of Defense
- Branch
- Missile Defense Agency
- Recipient company
- METAL MATRIX CAST COMPOSITES, LLC (DBA M
- Proposal award date
- 2005-04-25
- Contract end date
- 2005-10-24
- UEI
- Not reported
- Solicitation number
- 2004.4
- Topic code
- MDA04-139
Research abstract
A manufacturing technique is developed to strategically embed thermal pyrolytic graphite (TPG) insert into copper graphite composite. TPG will then be located in the critical thermal path of phase array radar antenna slat so that the slat is allowed to be cooled from its edge. The enhancement of thermal performance by TPG insertion allows the antenna slat to be cooled at its edge while the advanced wide band gap semiconductors, such as GaN and SiC, are used in the microwave modules. At an average heat flux of 100 W/cm2, which is assumed at the module level for GaN devices, the temperature difference along the thermal path of 1.5" long, in the case of copper graphite composite, from module mounting surface to cooling fins was estimated as only 8 °C, using a simplified one-dimensional heat transfer method. This temperature drop is adequate for the total thermal management of GaN devices whose junction temperature can be as high as 250 °C.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Thermal Pyrolytic Graphite Embedded Copper Graphite and Aluminum Graphite Composites for Thermal Management of Phase Array Radar Systems
- Micro-channel/Low Profile Heat Spreader
- Micro-channel/Low Profile Heat Spreader
- Active Radar System Thermal Management
- High Thermal Conductivity, CTE Matched Heat Spreader with MicroChannel Structures