
Hyper-Therm High-Temperature Composites (AKA: Hyper-Therm Inc) Profile last edited on: 11/14/2018
CAGE: 0W5H1
UEI: WRLGUJSGKJG8
Business Identifier: Ceramic matrix composites Is this YOUR Company?
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Location Information
Location: Single
Congr. District: 48
County: Orange
Congr. District: 48
County: Orange
Public Profile
in 2013, Rolls-Royce, the global power systems company, acquired Hyper-Therm High Temperature Composites, Inc., a producer of state-of-the-art composite materials, including ceramic matrix composites (CMCs), engineered coatings and thermal-structural components. Hyper-Therm HTC will become a wholly-owned subsidiary of Rolls-Royce, and will serve as the hub for technical development of CMCs, which will find applications in a broad range of future Rolls-Royce power systems.Hyper-Therm High-Temperature Composites uses patented Chemical Vapor Infiltration/Deposition (CVI/CVD) process technology. The use of these new materials in gas turbine engine components offer the benefits of strength at higher temperatures to reduce the requirement for cooling air. CMCs are also typically one third of the density of nickel super alloys which could significantly reduce the weight of components. This would mean more environmentally friendly engines with improved efficiency and reduced emissions.
Extent of SBIR involvement
Synopsis: Awardee Business Condition
Employee Range
20-24Revenue Range
2M-2.5MVC funded?
NoPublic/Private
Privately HeldStock Info
----IP Holdings
1-4Awards Distribution by Agency
Most Recent SBIR Projects
Year | Phase | Agency | Total Amount | |
---|---|---|---|---|
2013 | 1 | DOE | $148,857 | |
Project Title: Ceramic Matrix Composites for Concentrating Solar Power Receivers | ||||
2011 | 2 | AF | $849,134 | |
Project Title: Ceramic Matrix Composite (CMC) Low Pressure Turbine (LPT) Blade Development | ||||
2011 | 1 | NASA | $99,998 | |
Project Title: Novel Fabrication Approach for SiC/SiC Thermal Protection System Elements | ||||
2011 | 2 | NASA | $691,631 | |
Project Title: SiC Matrix Composites for High Temperature Hypersonic Vehicle Applications | ||||
2010 | 2 | Navy | $777,709 | |
Project Title: Innovative Approaches for Evaluating Interlaminar Tensile Strength of Ceramic Matrix Composites (CMCs) at Elevated Temperatures |
Key People / Management
Wayne S Steffier -- President
Todd Z Engel
Tony Magaldi
Charlene F Rusnak
Robert J Shinavski
Todd Z Engel
Tony Magaldi
Charlene F Rusnak
Robert J Shinavski
Company News
There are no news available.