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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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Metallic Joining to Advanced Ceramic Composites
Amount: $125,000.00Currently, advanced ceramic composites are state-of-the-art for hypersonic airbreathing and space propulsion applications. The Launch Abort System (LAS) of the Orion Multi-Crew Exploration Vehicle (MC ...
SBIRPhase I2015National Aeronautics and Space Administration -
Advanced Zirconium Carbide Tie-Tubes for NTP
Amount: $125,000.00Nuclear Thermal Propulsion (NTP) has been identified as a critical technology needed for human missions to Mars due to its increased specific impulse (Isp) as compared to traditional chemical propulsi ...
SBIRPhase I2015National Aeronautics and Space Administration -
Oxidation Resistant Heating Elements for High Temperature Wind Tunnels
Amount: $749,999.00ABSTRACT: 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 28 ...
SBIRPhase II2015Department of Defense Air Force -
Non-Eroding Hot Gas Components for Strategic Propulsion Systems Produced by Reduced Cost, Rapid Manufacturing Techniques
Amount: $150,000.00Innovative solutions are sought to reduce cost and lead-time of hot gas valve components located in the post boost control system (PBCS) of the U.S. Navys Trident II D-5 Fleet Ballistic Missile. Curre ...
SBIRPhase I2014Department of Defense Navy -
Breakdown Resistant Refractory Metal Coatings for Field-Aligned ICRF Antennas
Amount: $150,000.00In fusion plasmas, ion cyclotron range of frequency (ICRF) and lower hybrid range of frequency (LHRF) power is anticipated to be a primary auxiliary heating and current drive sources in next step toka ...
SBIRPhase I2014Department of Energy -
High Strength, Oxidation Resistant Fuel Claddings for Improved Accident Tolerance
Amount: $150,000.10The recent events at the Fukushima nuclear power plant highlight the need for enhanced accident tolerance. Of particular concern is the overheating of standard zirconium alloy cladding material in a l ...
SBIRPhase I2014Department of Energy -
Thermal Isolation of Solid Rocket Motor Exit Cone and Nozzle
Amount: $973,887.00Primary missile structures, ancillary mechanical and electrical sub-components of missile propulsion systems must be thermally isolated from hot propulsion gases. Silica-cloth phenolic and carbon-cl ...
SBIRPhase II2014Department of Defense Missile Defense Agency -
100-lbf Non-Toxic Storable Liquid Propulsion
Amount: $125,000.00NASA's Road Maps for both Launch and In Space Propulsion call for the development of non-toxic, monopropellant reaction control systems to replace current state-of-art hydrazine. The Orion Multi-Purp ...
SBIRPhase I2014National Aeronautics and Space Administration -
Reduced Cost Composite Hot Structures with Oxidation Protection
Amount: $125,000.00Innovative, low cost high performance technologies are critical to the affordability of future space missions. Carbon/carbon (C/C) composites have significant advantages over metallic solutions. Howe ...
SBIRPhase I2014National Aeronautics and Space Administration -
Fine Grained Tungsten Claddings for Cermet Based NTP Systems
Amount: $750,000.00In 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 II2014National Aeronautics and Space Administration
