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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. Electrolytic Decomposition and Ignition of AF-M315E Monopropellant

    Amount: $80,000.00

    Ionic liquid monopropellants such as AF-M315E offer many advantages over monopropellant hydrazine and nitrogen tetroxide/monomethyl hydrazine (NTO/MMH) bipropellant, including increased specific impul ...

    SBIRPhase I2015Department of Defense Navy
  2. 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 ...

    SBIRPhase I2014Department of Energy
  3. 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 ...

    SBIRPhase II2014Department of Energy
  4. 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 ...

    SBIRPhase I2014National Aeronautics and Space Administration
  5. 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 ...

    SBIRPhase I2014National Aeronautics and Space Administration
  6. 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 ...

    SBIRPhase I2014National Aeronautics and Space Administration
  7. 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 ...

    SBIRPhase I2014National Aeronautics and Space Administration
  8. 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 ...

    SBIRPhase I2014National Aeronautics and Space Administration
  9. 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 ...

    SBIRPhase II2014National Aeronautics and Space Administration
  10. Ductile Tungsten Alloy using Low-Activation Alloying Elements

    Amount: $150,000.00

    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 ...

    SBIRPhase I2013Department of Energy
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