High Temperature Corrosion Resistant Nanocomposite Materials for Turbine Engine Applications

Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: W31P4Q-07-C-0036
Agency Tracking Number: 06SB2-0064
Amount: $99,000.00
Phase: Phase I
Program: SBIR
Awards Year: 2006
Solicitation Year: 2006
Solicitation Topic Code: SB062-003
Solicitation Number: 2006.2
Small Business Information
2721-D Merrilee Drive, Fairfax, VA, 22031
DUNS: 167433531
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: Y
Principal Investigator
 James Intrater
 Chief Engineer
 (703) 560-1371
Business Contact
 T. Sudarshan
Title: President
Phone: (703) 560-1371
Email: sudarshan@matmod.com
Research Institution
The operating temperature and efficiency of turbine engines is limited by the thermal properties of the coatings that are used to protect the underlying superalloys. Additionally, surface deposits that penetrate through the thermal barrier coating (TBC) system cause hot corrosion and premature failure of the coating. In order to extend the operational temperature and life of the turbines, a systems approach to develop new or improved coatings are required. The proposed effort by Materials Modification, Inc., will develop a nanocomposite coating system that is designed by taking into consideration the thermodynamic compatibility of the bond coat and the TBC along with minimizing thermal transport through the coating.

* information listed above is at the time of submission.

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