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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. 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
  2. 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
  3. 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
  4. 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
  5. Ceramic Matrix Composite Fins and Nosetips for Gun-Launched Projectiles

    Amount: $225,000.00

    Boeing Defense Systems is developing a guided hypervelocity projectile (HVP) and associated integrated launch package assembly. The nosetip and fixed and rotating fin components present particular cha ...

    SBIRPhase I2019Department of Defense Office of the Secretary of Defense
  6. 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
  7. 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
  8. Microengineered Textured Armor for Plasma-Facing Components

    Amount: $999,998.00

    Application of nuclear fusion for cost-competitive energy generation cannot be realized until advanced plasma- facing materials and structures are developed. The specific problem addressed in this pro ...

    SBIRPhase II2018Department of Energy
  9. High-Efficiency System for Dry Heat Rejection

    Amount: $150,000.00

    Dry cooling systems are the only option for industrial and utility power plants that are unable to obtain cooling water supplies or permits, and can be applied to both nuclear- and fossil-fueled plant ...

    SBIRPhase I2018Department of Energy
  10. Advanced Ignition System for Hybrid Rockets for Mars Sample Return, Phase II

    Amount: $749,715.00

    To return a sample from the surface of Mars or any of the larger moons in the solar system will require a propulsion system with a comparatively large delta-V capability. Consequently, significant pro ...

    SBIRPhase II2018National Aeronautics and Space Administration
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