REACTION SYSTEMS, INC
Address
Information
| DUNS: | 196231166 |
| # of Employees: | 7 |
Ownership Information
| Hubzone Owned: | N |
| Socially and Economically Disadvantaged: | N |
| Woman Owned: | N |
Award Charts
Award Listing
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Record 1 TO 18
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Using the Conditional Moment Closure Method to Assess the Effects of Turbulence Chemical Kinetics
Amount: $149,992.00The ability to accurately design and predict the performance of combustion-based machinery like gas turbine engines is important in improving their performance, increasing their fuel economy, lowering ...
STTRPhase I2016Department of Defense Army -
An Advanced Endothermic Fuel System for Hypersonic Propulsion
Amount: $749,996.00ABSTRACT: 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 ...
SBIRPhase II2015Department of Defense Air Force -
A Novel Thermal Method for Rapid Coke Measurement in Liquid Rocket Engines
Amount: $746,565.00ABSTRACT: 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 ...
SBIRPhase II2013Department of Defense Air Force -
An Advanced Endothermic Fuel System for Hypersonic Propulsion
Amount: $149,998.00ABSTRACT: 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 ...
SBIRPhase I2013Department of Defense Air Force -
Advanced Supported Liquid Membranes for CO2 Control in EVA Applications
Amount: $750,000.00The 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 ...
SBIRPhase II2012National Aeronautics and Space Administration -
A Novel Thermal Method for Rapid Coke Measurement in Liquid Rocket Engines
Amount: $150,000.00ABSTRACT: 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 ...
SBIRPhase I2012Department of Defense Air Force -
Self-Organizing Maps for Fast LES Combustion Modeling
Amount: $99,997.00Tremendous 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 ...
SBIRPhase I2011National Aeronautics and Space Administration -
Advanced Supported Liquid Membranes for CO2 Control in EVA Applications
Amount: $100,000.00The 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 ...
SBIRPhase I2011National Aeronautics and Space Administration -
Catalytic N2O Decomposition for Piloted Scramjet Ignition
Amount: $806,442.00High 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 ...
SBIRPhase II2010Department of Defense Air Force -
A Novel Process for Improved Hydrogen Separation and Recovery
Amount: $100,000.00Because 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 ...
SBIRPhase I2010Department of Energy
