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Plasma Processes, LLC

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


http://plasmapros.com

Information

UEI: KAWTP8XNFEK9

# of Employees: 44


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Green Monopropellant Propulsion for Small Spacecrafts

    Amount: $125,000.00

    One of the biggest obstacles preventing the widespread implementation of small satellites is the process of actually getting them into space. Current methods include hitching rides as secondary payloa ...

    SBIRPhase I2016National Aeronautics and Space Administration
  2. Further Enhancement of Non-Eroding Throat Liner Technology to Enable TSRM

    Amount: $1,498,494.00

    Plasma Processes non-eroding throat (NET) technology for aluminized propellants has been significantly matured since 1999.A recent full-scale second stage motor test demonstrated that the technology h ...

    SBIRPhase II2016Department of Defense Missile Defense Agency
  3. Electro-Catalytic Propulsion System for Ionic Propellants

    Amount: $80,000.00

    Current propellant systems aboard NAVY ships and submarines are restricted to solid propellant Divert and Attitute Control Systems (DACS) or Throttleable DACS (TDACS) due to the high toxicity, reactiv ...

    SBIRPhase I2016Department of Defense Navy
  4. Non-Eroding Post-Boost Control Hot Gas Components Produced by Rapid Manufacturing Techniques

    Amount: $749,985.00

    Innovative solutions are sought to reduce cost, lead-time and improve capability of hot gasmanagement components in the post boost control system (PBCS) of the U.S. Navys Trident IID-5 Fleet Ballistic ...

    SBIRPhase II2016Department of Defense Navy
  5. 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 ...

    SBIRPhase I2015Department of Defense Missile Defense Agency
  6. 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 ...

    SBIRPhase I2015Department of Energy
  7. High Density, Multi-Layered Nosetips for Hypersonic Projectiles

    Amount: $1,411,960.00

    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 ...

    SBIRPhase II2015Department of Defense Navy
  8. 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 ...

    SBIRPhase II2015Department of Energy
  9. 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 ...

    SBIRPhase II2015National Aeronautics and Space Administration
  10. 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 ...

    SBIRPhase I2015National Aeronautics and Space Administration
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