You are here
REACTION SYSTEMS, INC
http://www.reactionsystemsllc.com
UEI: RSALD9ULYWG3
# of Employees: 7
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
-
Chemical Kinetic Pathway Effects in Turbulent Reacting Flows
Amount: $998,832.00The Army is very interested in accurate simulations of combustion in devices such as rockets and gas turbines, Otto and Diesel cycle IC engines, scramjet engines, rotating detonation engines, etc.The ...
STTRPhase II2017Department of Defense Army -
An Advanced Facilitated Transport Membrane for CO2 Capture from Dilute Streams
Amount: $150,000.00Coal-fired power plants generate 45% of the electricity in the United States and they are also a major source of CO2 emissions. Low- cost processes for CO2 capture are being developed but these leave ...
SBIRPhase I2016Department of Energy -
Advanced Supported Liquid Membranes for Ammonia and Formaldehyde Control in Spacesuits
Amount: $124,999.00With plans to transition to the Rapid Cycle Amine system for CO2 control in the Portable Life Support System used for extra vehicular activities (EVA), NASA has a need to improve the method for contro ...
SBIRPhase I2016National Aeronautics and Space Administration -
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: $1,472,736.00ABSTRACT: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 syste ...
SBIRPhase II2014Department 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
