Ultramet

Basic Information

12173 Montague Street
Pacoima, CA, 91331-2210

http://www.ultramet.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 95
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 70


  1. Advanced Heat Exchangers for Dry-Cooling Systems

    Amount: $150,000.00

    Dry cooling systems are currently the only option for industrial and utility power plants that are unable to obtain permits for cooling water. Dry cooling systems are higher cost and less efficient th ...

    SBIR Phase I 2014 Department of Energy
  2. Ductile Tungsten Alloy Using Low-Activation Alloying Elements

    Amount: $999,990.00

    Designs for the International Thermonuclear Experimental Reactor (ITER) employ several plasma-facing materials selected for their suitability to regions of the vessel with different power and flux cha ...

    SBIR Phase II 2014 Department of Energy
  3. Advanced Ceramic Matrix Composite Leading Edge Materials and Processing for Hypersonic Vehicles

    Amount: $150,000.00

    ABSTRACT: In previous work for MDA and the Army, Navy, and Air Force, Ultramet demonstrated the fabrication of carbon fiber-reinforced refractory carbide matrix composites for missile and railgun pro ...

    SBIR Phase I 2014 Air Force Department of Defense
  4. Advanced Foam-Based Cryogenic Heat Exchanger, Phase II

    Amount: $749,937.00

    In the Phase I project, Ultramet designed, modeled, fabricated, and tested a compact foam-based cryogenic heat exchanger for use as part of a superconducting degaussing system. Several heat exchanger ...

    SBIR Phase II 2014 Department of Defense Navy
  5. Continued Optimization of Low-Density Foam-Reinforced Ablatives for High-Velocity, High Heat Flux Earth Return Missions, Phase II

    Amount: $750,000.00

    In previous work for NASA, Ultramet and ARA Ablatives Laboratory developed and demonstrated advanced foam-reinforced carbon/phenolic ablators that offer substantially increased performance under high ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  6. High Heat Flux Block Ablator-In-Honeycomb Heat Shield Using Ablator/Aerogel-Filled Foam

    Amount: $125,000.00

    Ultramet and ARA Ablatives Laboratory previously developed and demonstrated advanced foam-reinforced carbon/phenolic ablators that offer substantially increased high heat flux performance and reduced ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  7. Laser-Directed CVD 3D Printing of Refractory Metal Rocket Propulsion Hardware

    Amount: $125,000.00

    In this project, Ultramet will develop a three-dimensional (3D) laser-directed chemical vapor deposition (CVD) additive manufacturing system to build free-form refractory metal structures for liquid r ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  8. O2/CO Ignition System for Mars Sample Return Missions

    Amount: $125,000.00

    Returning a geological sample from the surface of Mars will require an ascent propulsion system with a comparatively large velocity change (delta-V) capability due to the relatively deep Martian gravi ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  9. Ultralightweight Refractory-Lined C/C Ascent Engine Combustion Chambers

    Amount: $125,000.00

    Mars sample return ascent vehicles require a velocity change exceeding 4 km/s within minutes of launch and higher propellant mass fractions than are offered by current pressure-fed satellite propulsio ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  10. Fabrication and Testing of Nuclear-Thermal Propulsion Ground Test Hardware

    Amount: $125,000.00

    Efficient nuclear-thermal propulsion requires heating a low molecular weight gas, typically hydrogen, to high temperature and expelling it through a nozzle. The higher the temperature and pressure, th ...

    SBIR Phase I 2014 National Aeronautics and Space Administration

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