Hyper-Therm High-Temperature Composites

Address

CA
Unit B
Huntington Beach, CA, 92648-1208

http://www.htcomposites.com

Information

DUNS: 798073391
# of Employees: 15

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  1. Ceramic Matrix Composites for Concentrating Solar Power Receivers

    Amount: $148,857.00

    Concentrating Solar Power (CSP) offers significant potential as a clean an inexhaustible utility- scale energy source to meet ever-increasing global and domestic energy demands. Most CSP power generat ...

    SBIRPhase I2013Department of Energy
  2. SiC Matrix Composites for High Temperature Hypersonic Vehicle Applications

    Amount: $591,631.00

    Durable high temperature materials are required for reusable hypersonic structural thermal protection systems. In particular, temperatures exceeding 2700ºF, and approaching 3000ºF, are targeted for ...

    SBIRPhase II2011National Aeronautics and Space Administration
  3. Novel Fabrication Approach for SiC/SiC Thermal Protection System Elements

    Amount: $99,998.00

    Durable high temperature materials are required for structural thermal protection systems (TPS) that exhibit a structural load carrying capability at temperatures in excess of 2700ºF. Fabrication t ...

    SBIRPhase I2011National Aeronautics and Space Administration
  4. Ceramic Matrix Composite Low Pressure Turbine Blade Development

    Amount: $749,134.00

    Although the turbine engine has revolutionized both military and commercial aircraft, future requirements for more capable, durable, and cost-effective aircraft systems can only be achieved through ev ...

    SBIRPhase II2011Department of Defense
  5. SiC Matrix Composites for High Temperature Hypersonic Vehicle Applications

    Amount: $100,000.00

    Durable high temperature materials are required for hypersonic engine and structural thermal protection systems. In particular, 2700ºF or greater capable structural materials that can survive stress ...

    SBIRPhase I2010National Aeronautics and Space Administration
  6. High Efficiency SiC/SiC Composite Heat Exchanger Structures

    Amount: $98,187.00

    Scramjet propulsion systems for future hypersonic aerospace vehicles will be subjected to heating rates far greater than current materials can manage. In order to sustain high thermal loading while pr ...

    SBIRPhase I2010National Aeronautics and Space Administration
  7. High-Temperature, Full-Field Strain Mapping of Ceramic Matrix Composites for Aero-Engine Components

    Amount: $100,000.00

    Continuous fiber-reinforced ceramics are an emerging class of materials that offer considerable potential for increasing weight-specific performance while reducing fuel consumption and enhancing the d ...

    SBIRPhase I2010Air Force Department of Defense
  8. Innovative Approach for Evaluating Interlaminar Tensile Strength of Ceramic Matrix Composites at Elevated Temperatures

    Amount: $627,728.00

    Hot structures fabricated from ceramic composite materials are an attractive design option for components of future high-speed aircraft and propulsion systems to reduce weight and increase performance ...

    SBIRPhase II2010Department of Defense
  9. Design Validation of Gen IV Composite Control Rod Sheaths

    Amount: $100,000.00

    The purpose of this proposed effort is to further advance the state of technology for Nuclear Grade SiC/SiC to make these composites the primary choice for fabricating highly irradiated, high temperat ...

    SBIRPhase I2010Department of Energy
  10. Low Erosion Ceramic Composite Liners for Improved Performance of Ablative Rocket Thrust Chambers

    Amount: $600,000.00

    Advanced liquid rocket propulsion systems must achieve longer burn times without performance degradation to allow the lowest cost per kilogram access to space. Ablative thrust chambers have an extensi ...

    STTRPhase II2009National Aeronautics and Space Administration

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