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Company Information
12173 Montague St
Pacoima, CA 91331-2210
United States


DUNS: 052405867

# of Employees: 67

Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N

Award Charts

Award Listing

  1. Design, Fabrication, and Testing of a High Temperature Foam Core Heat Exchanger for Small Modular Reactors

    Amount: $206,500.00

    A helium-cooled small modular reactor (SMR) can take advantage of the Brayton power conversion cycle with greater efficiency compared to the steam Rankine cycle. Alternatively, a more advanced supercr ...

    SBIRPhase I2020Department of Energy
  2. Compact Heat Exchangers for Space Power Systems

    Amount: $124,999.00

    For missions to dark, dusty, or distant destinations, solar power is not practical. General-purpose heat sources used in conjunction with a heat engine represent a viable solution. The critical challe ...

    SBIRPhase I2020National Aeronautics and Space Administration
  3. Advanced Horizontal CVD Reactor Development for Increased Process Efficiency to Produce Seamless Thick-Film CVD Niobium-Lined Copper SRF Cavities

    Amount: $206,500.00

    DOE is interested in innovative fabrication technologies for cost-effective high-Q, high-field superconducting radio frequency (SRF) cavities necessary for the economic viability of future accelerator ...

    SBIRPhase I2019Department of Energy
  4. Integration of TRISO Fuel Particles with Open-Cell Foam for Increased Safety, Heat Transfer, and Fuel Performance

    Amount: $206,500.00

    Tristructural isotropic (TRISO) fuel is a key component of advanced small modular nuclear fission reactors due to its inherent safety at high temperatures and irradiation levels and decreased prolifer ...

    STTRPhase I2019Department of Energy
  5. Coatings for Protection against Hot Hydrogen in Solar-Thermal Propulsion

    Amount: $125,000.00

    Advanced carbon-based heat exchangers (carbon/carbon composite or graphite) used in solar-thermal propulsion engines must be protected for extended periods from the ge;3000 K hydrogen propellant. In p ...

    SBIRPhase I2019National Aeronautics and Space Administration
  6. Design and Fabrication of a Mars Ascent Vehicle Reaction Control System

    Amount: $125,000.00

    Sample return missions generally have the largest velocity change (Delta;V) requirements for a mission to a given body such as Mars. For every pound of Mars liftoff mass removed from the return vehicl ...

    SBIRPhase I2019National Aeronautics and Space Administration
  7. Combustion Chambers for Use with AF-M315E Monopropellant

    Amount: $75,000.00

    The use of AF-M315E, a non-toxic monopropellant developed by the Air Force, promises substantial performance improvement and reduced cost compared with legacy hydrazine-based systems. Before the techn ...

    SBIRPhase I2019Department of Defense Air Force
  8. Characterization and Scaleup of High Temperature Oxidation-Resistant Coatings for Carbon/Carbon Composites

    Amount: $143,703.00

    Hypersonic flight performance of a lifting body vehicle design is improved significantly by the drag reduction achieved when nose and wing leading edges are sharp and shape-stable under all flight con ...

    SBIRPhase I2019Department of Defense Air Force
  9. Low-Density Ablator-Filled Foam Incorporating Lyocell-Derived Carbon Fiber for BMDS Interceptors, Phase II

    Amount: $996,716.00

    In previous exit cone insulator development for MDA and heat shield fabrication for NASA, Ultramet developed advanced foam-reinforced carbon/phenolic ablators, now at TRL 6, that offer substantially i ...

    SBIRPhase II2018Department of Defense Missile Defense Agency
  10. CVD Process Development of Thin Film Triniobium-Tin on Copper SRF Cavities

    Amount: $999,998.00

    Innovative fabrication technologies for cost-effective high-Q, high-field superconducting radio frequency (SRF) components are needed for the economic viability of future accelerator facilities. The w ...

    SBIRPhase II2018Department of Energy
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