You are here

ULTRAMET

Company Information
Address
12173 MONTAGUE ST
PACOIMA, CA 91331-2210
United States


http://www.ultramet.com

Information

UEI: N8ZRMWX85NZ6

# of Employees: 57


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Advanced Materials and Manufacturing for Low-Cost, High-Performance Liquid Rocket Combustion Chambers, Phase II

    Amount: $600,000.00

    Silicided niobium alloy (C103) combustion chambers have been used extensively in both NASA and DoD liquid rocket propulsion systems. Niobium alloys offer a good combination of temperature capability, ...

    SBIRPhase II2005National Aeronautics and Space Administration
  2. Advanced Tungsten Structures for Plasma-Facing Components in Magnetic Confinement Fusion Energy Reactors

    Amount: $99,989.00

    79191S The potential economic, environmental, and strategic benefits associated with the development of magnetic fusion energy (MFE) are numerous. However, fusion technology cannot be realized until ...

    SBIRPhase I2005Department of Energy
  3. Conformal Leading Edge Heat Pipe

    Amount: $99,999.00

    Aerothermal heating of leading edges and nose tips on reentry vehicles creates stagnation-point temperatures that are beyond the limits of most materials. For systems that have reusability requirement ...

    SBIRPhase I2005Department of Defense Air Force
  4. High-Performance Catalysts for Small Impulse Bit Thrusters, Phase II

    Amount: $600,000.00

    The current push to develop small satellites, the need for formation flying constellations, and the desire to replace reaction control wheels have resulted in the need for thrusters that can deliver v ...

    SBIRPhase II2005National Aeronautics and Space Administration
  5. Complex-Shaped SiC/SiC Ceramic Matrix Composites via Novel, Non-Woven Preforming

    Amount: $150,000.00

    The use of ceramic matrix composites (CMCs) has the potential to increase the life and operating envelope of turbine engines. While great strides have been made in mechanical properties, CMCs still su ...

    SBIRPhase I2005Department of Defense Navy
  6. Low-Cost, Low-Temperature Deposition of Fiber Interface Coatings

    Amount: $149,993.00

    Conventional fiber-matrix interface coatings applied by chemical vapor infiltration (CVI) are expensive because they require costly, high-temperature equipment and must be applied at a slow rate in or ...

    SBIRPhase I2005Department of Defense Navy
  7. Cost-Effective, High-Performance, High-Purity Niobium Superconducting Radio Frequency Cavities

    Amount: $99,998.00

    78163S Superconducting radio frequency (RF) accelerating cavities provide high continuous wave operating fields while offering higher beam quality and reduced beam-cavity interaction for high-energy ...

    SBIRPhase I2005Department of Energy
  8. Transpiration-Cooled Hydrocarbon-Fueled Scramjet Engine

    Amount: $99,996.00

    The Air Force is seeking advanced cooling concepts for scramjet engines for use in hypersonic cruise missiles, Mach 8-10 strike/reconnaissance aircraft, and affordable, on-demand access to space. In c ...

    SBIRPhase I2005Department of Defense Air Force
  9. Novel Low Temperature Coating Method for Environment-Resistant Coatings on Polymers

    Amount: $100,000.00

    Polybenzoxazole polymers, including polyphenylenebenzobisoxazole (PBO) in particular, are under development for use in a wide variety of aerospace applications due to their remarkable tensile strength ...

    SBIRPhase I2005Department of Defense
  10. Lightweight Ultrahigh Temperature CMC-Encased C/C Structure for Reentry and Hypersonic Applications

    Amount: $70,000.00

    The reentry spacecraft and hypersonic cruisers of the future will require advanced lightweight thermal protection systems that can provide the dual functionality of thermal protection and structural c ...

    SBIRPhase I2005National Aeronautics and Space Administration
US Flag An Official Website of the United States Government