MICRO COOLING CONCEPTS

Basic Information

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

Company Profile

n/a

Additional Details

Field Value
DUNS: 001557268
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 5


  1. 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 ...

    SBIR Phase I 2013 Department of Defense Air Force
  2. 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 ...

    SBIR Phase II 2012 National Aeronautics and Space Administration
  3. 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 ...

    SBIR Phase I 2012 Department of Defense Army
  4. 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 ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  5. 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 ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  6. 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 ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  7. 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 ...

    SBIR Phase I 2007 Army Department of Defense
  8. 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 ...

    SBIR Phase II 2006 Missile Defense Agency Department of Defense
  9. High Effectiveness Heat Exchanger for Cryogenic Refrigerators

    Amount: $69,756.00

    We propose an innovative high performance cryogenic heat exchanger manufactured of titanium by photo-etching and diffusion bonding. This is a parallel plate design of thin laminated titanium foils. Ti ...

    SBIR Phase I 2005 National Aeronautics and Space Administration
  10. Compact 10K Hybrid Cryocooler

    Amount: $97,726.00

    Long life mechanical cryocoolers for space applications have matured during the last decade, and 77 K and 35 K coolers are now available. However, 10 K equivalents are not available because fundamenta ...

    SBIR Phase I 2004 Missile Defense Agency Department of Defense

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