Engineered Materials for Advanced Gas Turbine Engine
This project will develop innovative composite powders and composites that will surpass the properties of currently identified materials for advanced gas turbine engine applications. Phase I will demonstrate a powder metallurgy technique for fabricating high-temperature, oxidation-resistant composite powders. Once consolidated, the resulting composite will possess high creep and thermal fatigue strength, and a low coefficient of thermal expansion properties.
Small Business Information at Submission:
Advanced Powder Solutions
14102 Halprin Creek Drive Cypress, TX 77429-6042
Number of Employees: