PLASMA PROCESSES, LLC

Basic Information

4914 MOORES MILL RD
HUNTSVILLE, AL, 35811-1558

http://plasmapros.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 799114574
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 28


  1. Further Enhancement of Non-Eroding Throat Liner Technology to Enable Upper Stage Solid Rocket Motor Transition

    Amount: $125,000.00

    Plasma Processes non-eroding throat liner technology for aluminized propellants has been significantly matured since 1999. An upcoming full-scale test will demonstrate that the technology is sufficien ...

    SBIR Phase I 2015 Department of Defense Missile Defense Agency
  2. Mitigation of Radio Frequency Breakdown Using Refractory Metal Coatings

    Amount: $150,000.00

    Obtaining high-gradient, high frequency accelerator structures are essential for future science, medicine and biology, energy and environment, and national security applications. Emerging experimenta ...

    SBIR Phase I 2015 Department of Energy
  3. High Density, Multi-Layered Nosetips for Hypersonic Projectiles

    Amount: $478,324.00

    The 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 ...

    SBIR Phase II 2015 Department of Defense Navy
  4. Breakdown Resistant Refractory Metal Coatings for Field-Aligned ICRF Antennas

    Amount: $1,000,000.00

    In 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 ...

    SBIR Phase II 2015 Department of Energy
  5. 100-lbf Non-Toxic Storable Liquid Propulsion

    Amount: $749,902.00

    NASA's Road Maps for both Launch and In Space Propulsion call for the development of non-toxic, monopropellant reaction control systems to replace the current toxic hydrazine based systems. The Orion ...

    SBIR Phase II 2015 National Aeronautics and Space Administration
  6. Thermo-Catalytic Ignition of Cryogenic Oxygen-Methane

    Amount: $125,000.00

    Liquid oxygen and methane propellants for in space chemical propulsion of future space exploration vehicles is desired for increased performance and elimination of toxicity of conventional hypergolic ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  7. Metallic Joining to Advanced Ceramic Composites

    Amount: $125,000.00

    Currently, 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 ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  8. Advanced Zirconium Carbide Tie-Tubes for NTP

    Amount: $125,000.00

    Nuclear 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 ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  9. Non-Eroding Hot Gas Components for Strategic Propulsion Systems Produced by Reduced Cost, Rapid Manufacturing Techniques

    Amount: $150,000.00

    Innovative 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 ...

    SBIR Phase I 2014 Department of Defense Navy
  10. Breakdown Resistant Refractory Metal Coatings for Field-Aligned ICRF Antennas

    Amount: $150,000.00

    In 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 ...

    SBIR Phase I 2014 Department of Energy

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