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THERMACORE, INC.

Company Information
Address
780 EDEN RD OFC
LANCASTER, PA 17601-4276
United States


http://www.thermacore.com

Information

UEI: HUT3XNPLRL77

# of Employees: 185


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. A POROUS METAL COOLED KLYSTRON COLLECTOR

    Amount: $679,930.00

    THE OBJECTIVE OF THIS PROGRAM IS TO DEMOSTRATE THE CAPABILITY OF POROUS METAL COOLING TO EFFECTIVELY REMOVE HEAT ABSORBED BY A MULTI-STAGE DEPRESSED COLLECTOR OF HIGH POWER B-FACTORY KLYSTRONS. HEAT ...

    SBIRPhase II1995Department of Energy
  2. A Helium-Cooled Faraday Shield Using Porous Metal Cooling

    Amount: $74,929.00

    N/A

    SBIRPhase I1995Department of Energy
  3. Titanium-Lined Lunar Radiator Heat Pipes

    Amount: $69,973.00

    N/A

    SBIRPhase I1995National Aeronautics and Space Administration
  4. HEAT PIPE COOLING OF TURBOSHAFT ENGINES

    Amount: $664,997.00

    THE PROPOSED WORK PLAN WILL EXAMINE THE USE OF HEAT PIPE COOLING IN TURBOSHAFT ENGINES TO INCREASE PERFORMANCE BY REDUCING OR ELIMINATING THE COMPRESSOR DISCHARGE BLEED AIR REQUIRED TO COOL ENGINE COM ...

    SBIRPhase II1994Department of Defense Army
  5. IMPROVED FLEXIBLE HEAT PIPE COLD PLATE TECHNOLOGY FOR AIRCRAFT CONTROL

    Amount: $375,000.00

    The innovation is the incorporation of capillary pumped loop (CPL) heat pipe technology into Thermacore developed Flexible Heat Pipe Cold Plate (FHPCP) hardware. Thermacore has successfully designed, ...

    SBIRPhase II1994Department of Defense Air Force
  6. REDUCED-MASS RADIATOR USING HIGH-TEMPERATURE LOOP PIPES

    Amount: $60,014.00

    The innovation in the proposed program is the replacement of conventional heat pipes in the current design with Russian-designed and patented loop heat pipes. This significantly reduces the radiator m ...

    SBIRPhase I1994Department of Defense Missile Defense Agency
  7. Anti-Icing of Gas Turbine Engine Inlets

    Amount: $69,982.00

    In turboshaft and turbofan gas turbine engines, anti-icing of the cowl currently uses compressor discharge bleed air. Use of this air decreases the net thrust or shaft horsepower, and increases the fu ...

    SBIRPhase I1994National Aeronautics and Space Administration
  8. LONG LIFE COMPONENTS FOR AMTEC POWER SYSTEMS

    Amount: $59,016.00

    The Alkali Metal Thermal to Electric Converter (AMTEC) is a high temperature, high efficiency system for converting thermal to electrical energy, with no moving parts. Published conceptual design stud ...

    SBIRPhase I1994Department of Defense Air Force
  9. HYDROGEN PERMEATION BARRIERS FOR BIMODAL REACTORS

    Amount: $74,987.00

    BIMODAL SPACE NUCLEAR POWER SYSTEMS WHICH COMBINE BOTH THERMAL PROPULSION AND ELECTRIC POWER GENERATION CAPABILITIES IN A SINGLE INTEGRATED POWER AND PROPULSION PLATFORM HAVE RECENTLY EMERGED AS STRON ...

    SBIRPhase I1994Department of Energy
  10. Porous Cathode for Alkali Propellant MPD Thrusters

    Amount: $497,679.00

    N/A

    SBIRPhase II1994National Aeronautics and Space Administration
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