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REACTION SYSTEMS, INC.
http://www.reactionsystemsllc.com
UEI: RSALD9ULYWG3
# of Employees: 10
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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High Capacity RCA Sorbents for Increased Cycle Times
Amount: $149,810.00NASA is interested in improving the method to control CO2 and water in the Exploration Extravehicular Mobility Unit (xEMU) to meet the ambitious objectives of the Artemis program, which includes human ...
SBIRPhase I2022National Aeronautics and Space Administration -
Novel Methods to Mitigate Heat Exchanger Fouling
Amount: $499,949.00Current Navy ships make use of shell-and-tube heat exchangers, which can utilize seawater as a heat sink. This is advantageous since ships can easily pull in water, filter it, utilize the cooling capa ...
SBIRPhase II2022Department of Defense Navy -
An Advanced Endothermic Fuel System for Thermal Management in Hypersonic Vehicles
Amount: $749,996.00Air breathing hypersonic vehicles generate much greater heat loads than traditional aircraft and therefore the fuel must provide additional cooling from endothermic chemical reactions on top of that n ...
SBIRPhase II2021Department of Defense Air Force -
An Advanced Endothermic Fuel System for Thermal Management in Hypersonic Vehicles
Amount: $49,998.77Air breathing hypersonic vehicles generate much greater heat loads than traditional aircraft and therefore the fuel must provide additional cooling from endothermic chemical reactions on top of that n ...
SBIRPhase I2021Department of Defense Air Force -
1- Embedded Condition Monitoring for Digital Logistics and Maintenance
Amount: $239,985.00Current Navy ships make use of shell-and-tube heat exchangers, which can utilize seawater as a heat sink. This is advantageous since ships can easily pull in water, filter it, use it in a heat excha ...
SBIRPhase I2021Department of Defense Navy -
Active Shock Gradient Control for Scramjet Isolators
Amount: $139,920.00SWBLI (shock wave boundary layer interaction)2, SWBLI (shock wave boundary layer interaction)2, Hypersonics, fluidic injection, intake, flow control
SBIRPhase I2021Department of Defense Navy -
A CMC Approach to Modeling Unsteady Combustion in an Arbitrarily G-Loaded Solid Rocket Motor
Amount: $111,491.26The development of maneuvering Hypersonic Glide Vehicles (HGV’s) like the Russian Avangard system has highlighted the need to predict the trajectory of these weapons for interception as well as reen ...
SBIRPhase I2020Department of Defense Army -
Using the Conditional Moment Closure Method to Assess the Effects of Turbulence Chemical Kinetics
Amount: $1,099,998.00Predicting the emission signature and radar cross-section of rocket exhaust plumes is of vital interest to the Missile Defense Agency and U.S. Army to protect the U.S. homeland and our forces abroad. ...
STTRPhase II2020Department of Defense Army -
Catalytic N2O Decomposition for Piloted Scramjet Ignition
Amount: $1,500,000.00Achieving hypersonic flight with air breathing vehicles using logistics fuels is a demanding task. A significant challenge in the development of single use and reusable systems alike is ignition of th ...
SBIRPhase II2019Department of Defense Air Force -
A Supported Liquid Membrane System for Steady State CO2 Control in a Spacecraft Cabin
Amount: $124,985.00Reducing the allowable concentration of carbon dioxide (CO2) in spacecraft is a critical need for NASA. The system now used on the International Space Station (ISS) is the carbon dioxide removal asse ...
STTRPhase I2018National Aeronautics and Space Administration