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Plasma Processes, LLC
UEI: KAWTP8XNFEK9
# of Employees: 44
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Reduced Activation Tungsten for Fusion
Amount: $150,000.00Tungsten and its alloys are candidates for plasma facing component heat sinks and armor due to their low sputtering rate, high melting point, high thermal conductivity, high strength at elevated tempe ...
SBIRPhase I2013Department of Energy -
Thermal Isolation of Solid Rocket Motor Exit Cone and Nozzle
Amount: $149,998.00Current strategic solid rockets motors, such as the SM-3 third stage rocket motor (TSRM), employ highly aluminized propellants with gas temperatures of approximately 6,500F. Carbon-carbon nozzle thro ...
SBIRPhase I2013Department of Defense Missile Defense Agency -
Oxidation Resistant Heating Elements for High Temperature Wind Tunnels
Amount: $150,000.00ABSTRACT: High temperature wind tunnels are needed to replicate the environment vehicles will experience during high Mach number flight. Of particular interest are sustained airflow temperatures of ...
SBIRPhase I2013Department of Defense Air Force -
Fine Grained Tungsten Claddings for Cermet Based NTP Systems
Amount: $125,000.00In October 2011, NASA initiated the Nuclear Cryogenic Propulsion Stage (NCPS) program to evaluate the feasibility and affordability of Nuclear Thermal Propulsion (NTP). A critical aspect of the progr ...
SBIRPhase I2013National Aeronautics and Space Administration -
High Density Nosetips for Hypersonic Projectiles
Amount: $80,000.00The Navy is developing weapon systems capable of launching inert projectiles for long-range surface fire support and missile intercept applications. Inert projectiles offer significant logistical and ...
SBIRPhase I2013Department of Defense Navy -
Improved Rhenium Thrust Chambers for In-Space Propulsion
Amount: $900,000.00Radiation-cooled, bipropellant thrust chambers are being considered for the ascent/descent engines and reaction control systems for NASA missions such as Mars Sample Return and Orion MPCV. Currently, ...
SBIRPhase II2012National Aeronautics and Space Administration -
Non-Toxic HAN Monopropellant Propulsion
Amount: $894,427.00Non-toxic monopropellants have been developed that provide better performance than toxic hydrazine. Formulations based on hydroxylammonium nitrate (HAN) have superior performance as compared to hydraz ...
SBIRPhase II2012National Aeronautics and Space Administration -
Ultra High Temperature Hafnium-based Materials for Propulsion Technologies
Amount: $1,000,000.00Rhenium is the current material of choice for Divert and Attitude Control Systems (DACS) components of due to its erosion resistance, high-temperature strength and compatibility with propellant produc ...
SBIRPhase II2012Department of Defense Missile Defense Agency -
Improved Rhenium Thrust Chambers for In-Space Propulsion
Amount: $100,000.00Radiation-cooled, bipropellant thrust chambers are being considered for the ascent/descent engines and reaction control systems (RCS) for future NASA missions such as Mars Sample Return. Currently, i ...
SBIRPhase I2011National Aeronautics and Space Administration -
Non-Toxic HAN Monopropellant Propulsion
Amount: $100,000.00Non-toxic monopropellants have been developed that provide better performance than toxic hydrazine. Formulations based on hydroxylammonium nitrate (HAN) have superior performance as compared to hydraz ...
SBIRPhase I2011National Aeronautics and Space Administration
