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Plasma Processes, LLC

Company Information
4914 Moores Mill Road Unit D
Huntsville, AL 35811-1558
United States



# of Employees: 44

Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No

Award Charts

Award Listing

  1. Advanced Materials and Fabrication Techniques for the Orion Attitude Control Motor

    Amount: $100,000.00

    The Launch Abort System (LAS) for the Orion Crew Exploration Vehicle (CEV) will provide a safe escape for the crew in the event of an emergency during launch. A key component of the LAS is its Attitu ...

    STTRPhase I2009National Aeronautics and Space Administration
  2. Lightweight Nozzle Extension for Liquid Rocket Engines

    Amount: $600,000.00

    The ARES J-2X requires a large nozzle extension. Currently, a metallic nozzle extension is being considered with carbon-carbon composite as a backup. In Phase 1, Plasma Processes Inc. (PPI), with th ...

    SBIRPhase II2009National Aeronautics and Space Administration
  3. A Tailorable Structural Composite for GCR and Albedo Neutron Protection on the Lunar Surface

    Amount: $100,000.00

    A tailorable structural composite that will provide protection from the lunar radiation environment, including GCR and albedo neutrons will be developed. This composite will have increased structural ...

    SBIRPhase I2009National Aeronautics and Space Administration
  4. High Surface Iridium Anodes for Molten Oxide Electrolysis

    Amount: $100,000.00

    Processing of lunar regolith into oxygen for habitat and propulsion is needed to support future space missions. Direct electrochemical reduction of molten regolith is most attractive method of process ...

    SBIRPhase I2009National Aeronautics and Space Administration
  5. Multi-Use Coating for Abrasion Prevention, Wear Protection, and Lunar Dust Removal

    Amount: $100,000.00

    The deleterious effects of lunar dust, typically less than 50 µm in diameter, have to be addressed prior to establishing a human base and long duration human presence on the surface of the moon. Thes ...

    SBIRPhase I2009National Aeronautics and Space Administration
  6. Electrochemical Microalloying of Tungsten for Plasma Facing Component Applications

    Amount: $750,000.00

    Tungsten¿s inherent chemical inertness and high melting temperature make it an ideal heat sink and armor material for fusion applications. However, tungsten¿s intrinsic low temperature brittlen ...

    SBIRPhase II2009Department of Energy
  7. High Temperature Bond and Thermal Barrier Coatings

    Amount: $100,000.00

    The key to higher efficiencies and lower emissions in next generation power plants, such as Integrated Gasification Combined Cycle (IGCC) systems, is an increase in the firing temperatures that are no ...

    SBIRPhase I2009Department of Energy
  8. Light Weight Thrust Chambers for Advanced Interceptor Axial Propulsion

    Amount: $100,000.00

    The Network Centric Airborne Defense Element (NCADE) is an affordable boost- and ascent- phase ballistic missile interceptor system. NCADE has the same form, fit and interface as the Advanced Medium ...

    SBIRPhase I2008Department of Defense Missile Defense Agency
  9. Reduced Cost TaC-based Rocket Nozzle for Solid Boost Motors

    Amount: $100,000.00

    Missile defense interceptors will provide our nation with the capability of defeating threats to our homeland and our deployed troops. However, the fielding of these advanced interceptors is strongly ...

    SBIRPhase I2008Department of Defense Missile Defense Agency
  10. Lightweight Exit Cone for Liquid Rocket Engines

    Amount: $100,000.00

    The Pratt and Whitney Rocketdyne (PWR) J-2X engine will power the upper stage of the Ares I and the earth departure stage (EDS) of the Ares V, which will enable manned travels to the Moon and eventual ...

    SBIRPhase I2008National Aeronautics and Space Administration
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