MICRO COOLING CONCEPTS

Company Information
Address 7522 SLATER AVE STE 122
HUNTINGTON BEACH, CA, 92647-7738


Information

DUNS: 001557268

# of Employees: 5


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Anisotropic Ceramic-Metal Heat Exchanger for Cryogenic Applications

    Amount: $79,667.00

    DC cryogenic flow systems such as Joule-Thomson (JT) or turbo-Brayton require very high effectiveness heat exchangers to reduce input power, while also requiring the heat exchangers to have low SWaP-C ...

    SBIRPhase I2016Department of Defense Navy
  2. Injector-Integrated Fuel-Air Heat Exchanger Module

    Amount: $124,950.00

    Modern high efficiency gas turbine engines typically operate with hot section temperatures so high that metal parts in those areas need to be cooled to maintain strength and life properties. A well-es ...

    SBIRPhase I2016National Aeronautics and Space Administration
  3. Enhanced High Pressure Turbine Blade Cooling Architecture

    Amount: $149,128.00

    ABSTRACT: Next generation military unmanned aircraft have a need for lower thrust specific fuel consumption (TSFC) and higher power-to-weight ratio, exceeding the capability of current engines in thi ...

    SBIRPhase I2013Department of Defense Air Force
  4. Microtextured Surfaces for Turbine Blade Impingement Cooling

    Amount: $746,314.00

    Gas turbine engine technology is constantly challenged to operate at higher combustor outlet temperatures. In a modern gas turbine engine, these temperatures can exceed the blade and disk material lim ...

    SBIRPhase II2012National Aeronautics and Space Administration
  5. Lightweight Recuperators for Small Turbine Engines

    Amount: $99,102.00

    Turbine engines can significantly reduce fuel consumption by using a recuperator to heat compressor discharge air with heat from combustion exhaust gases. This increased fuel efficiency is offset by t ...

    SBIRPhase I2012Department of Defense Army
  6. Advanced Turbine Blade Cooling Techniques

    Amount: $99,321.00

    Gas turbine engine technology is constantly challenged to operate at higher combustor outlet temperatures. In a modern gas turbine engine, these temperatures can exceed the blade and disk material lim ...

    SBIRPhase I2011National Aeronautics and Space Administration
  7. Low Mass, Aluminum NOFBX Combustion Chamber Development

    Amount: $99,422.00

    Our team proposes to define a diffusion bonding process for aluminum as an enabling step to ultimately develop an innovative, lightweight, long life, aluminum combustion chamber technology for Non-tox ...

    SBIRPhase I2011National Aeronautics and Space Administration
  8. Microplate Heat Exchanger

    Amount: $99,358.00

    We propose a microplate heat exchanger for cryogenic cooling systems used for continuous flow distributed cooling systems, large focal plane arrays, multiple cooling locations, and very low vibration ...

    SBIRPhase I2010National Aeronautics and Space Administration
  9. Self Contained Two-Phase Thermal Management System

    Amount: $69,046.00

    Thermal management is a growing problem in all areas of military systems, due to increased use of electronic systems, and more stringent requirements on efficiency, size, and weight. In the case of ne ...

    SBIRPhase I2007Army Department of Defense
  10. Advanced Cold Head Manufacturing Techniques

    Amount: $696,140.00

    Applications for long life cryocoolers include missile detecting and tracking, space and ground surveillance, mapping, weather monitoring, supercomputers/workstations, Earth resources monitoring, astr ...

    SBIRPhase II2006Missile Defense Agency Department of Defense

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