REACTION SYSTEMS, INC

Basic Information

17301 W COLFAX AVE STE 160
GOLDEN, CO, 80401-4886

http://www.reactionsystemsllc.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 196231166
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 7


  1. An Advanced Endothermic Fuel System for Hypersonic Propulsion

    Amount: $749,996.00

    ABSTRACT: The development of weapons that can travel at hypersonic speeds is becoming a high priority to the US Air Force. A key technology needed for the continued development of these propulsion s ...

    SBIR Phase II 2014 Department of Defense Air Force
  2. A Novel Thermal Method for Rapid Coke Measurement in Liquid Rocket Engines

    Amount: $746,565.00

    ABSTRACT: The surfaces of rocket engines are exposed to high pressure combustion products at temperatures up to 6000°F. Regenerative cooling can cause coke to form on the heat exchanger surfaces an ...

    SBIR Phase II 2013 Department of Defense Air Force
  3. An Advanced Endothermic Fuel System for Hypersonic Propulsion

    Amount: $149,998.00

    ABSTRACT: The development of weapons that can travel at hypersonic speeds is becoming a high priority to the US Air Force. Continued development of these vehicles relies on the ability to cool the c ...

    SBIR Phase I 2013 Department of Defense Air Force
  4. Advanced Supported Liquid Membranes for CO2 Control in EVA Applications

    Amount: $750,000.00

    The development of new, robust, lightweight systems for CO2 removal during EVA is a crucial need for NASA. Current activity is focused on extending mission times without increasing the size and weigh ...

    SBIR Phase II 2012 National Aeronautics and Space Administration
  5. A Novel Thermal Method for Rapid Coke Measurement in Liquid Rocket Engines

    Amount: $150,000.00

    ABSTRACT: The surfaces of rocket engine thrust chambers, throats and nozzles are exposed to combustion products at temperatures ranging from 4000 to 6000 degrees F and therefore engines must utilize ...

    SBIR Phase I 2012 Department of Defense Air Force
  6. Self-Organizing Maps for Fast LES Combustion Modeling

    Amount: $99,997.00

    Tremendous advances have been made in the development of large and accurate detailed reaction chemistry models for hydrocarbon fuels. Comparable progress has also been achieved in CFD as an engineeri ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  7. Advanced Supported Liquid Membranes for CO2 Control in EVA Applications

    Amount: $100,000.00

    The development of new, robust, lightweight systems for CO2 removal during EVA is a crucial need for NASA. With current and anticipated space activities, mission times will need to be extended withou ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  8. Catalytic N2O Decomposition for Piloted Scramjet Ignition

    Amount: $806,442.00

    High speed air breathing engines can deliver payloads with vehicles that are smaller and lighter than rocket powered vehicles. Unfortunately, ignition and flame holding in scramjet engines has proven ...

    SBIR Phase II 2010 Department of Defense Air Force
  9. A Novel Process for Improved Hydrogen Separation and Recovery

    Amount: $100,000.00

    Because of increasing demand for energy and decreasing supply of fossil fuels there now is a strong need to reduce fossil fuel consumption and one way to do this is to use more efficient methods to co ...

    SBIR Phase I 2010 Department of Energy
  10. Novel Liquid Membranes for CO2 and H20 Control in EVA Applications

    Amount: $100,000.00

    The development of new, robust, lightweight systems for CO2 removal during EVA is a crucial need for NASA. With current activity focused on the development of Lunar outposts, mission times will need ...

    SBIR Phase I 2009 National Aeronautics and Space Administration

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