Basic Information

HUNTSVILLE, AL, 35811-1558

Point of Contact Information

Field Value
Business Official:
Firm CFO (or equivalent):
POC Contracting Officer (or equivalent)

Additional Details

Field Value
SBC Control ID: SBC_000001603
DUNS: 799114574
SIC Codes: n/a
NAICS Codes: n/a

Company Profile


  1. 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
  2. Non-Eroding Hot Gas Components for Strategic Propulsion Systems Produced by Reduced Cost, Rapid Manufacturing Techniques

    Amount: $80,000.00

    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. Navy"s Trident II D-5 Fleet Ballistic Missile. ...

    SBIR Phase I 2014 NavyDepartment of Defense
  3. 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
  4. High Strength, Oxidation Resistant Fuel Claddings for Improved Accident Tolerance

    Amount: $150,000.10

    The 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 ...

    SBIR Phase I 2014 Department of Energy
  5. Thermal Isolation of Solid Rocket Motor Exit Cone and Nozzle

    Amount: $973,887.00

    Primary 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 ...

    SBIR Phase II 2014 Missile Defense AgencyDepartment of Defense
  6. 100-lbf Non-Toxic Storable Liquid Propulsion

    Amount: $125,000.00

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

    SBIR Phase I 2014 National Aeronautics and Space Administration
  7. Reduced Cost Composite Hot Structures with Oxidation Protection

    Amount: $125,000.00

    Innovative, 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 ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  8. Fine Grained Tungsten Claddings for Cermet Based NTP Systems

    Amount: $750,000.00

    In 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 ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  9. 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 sufficie ...

    SBIR Phase I 2014 Department of DefenseMissile Defense AgencyDepartment of Defense
  10. Reduced Activation Tungsten for Fusion

    Amount: $150,000.00

    Tungsten 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 ...

    SBIR Phase I 2013 Department of Energy

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