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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. Flow Channel Inserts Based on Syntactic Closed-Cell SiC Foam for Dual-Coolant ITER Test Blanket Modules

    Amount: $100,000.00

    The International Thermonuclear Experimental Reactor (ITER) design requires the development of advanced materials for flow channel inserts, in order to permit the high tritium breeder exit temperature ...

    SBIRPhase I2008Department of Energy
  2. High-Toughness Tungsten Alloys for Plasma Facing Components

    Amount: $100,000.00

    Tungsten is one of the most important candidate materials for the diverter components of fusion energy systems, due to its low erosion and good properties at high temperature. However, the fabrication ...

    SBIRPhase I2008Department of Energy
  3. Advanced Foam Core Composite Insulation for Extended Range Hypersonic Vehicles

    Amount: $100,000.00

    Hypersonic flight requires the development of insulating materials with a combination of thermal conductivity, density, and structural integrity that is beyond the capability of materials currently in ...

    SBIRPhase I2007Department of Defense Air Force
  4. Economical Manufacture of Refractory Ceramic Matrix Composite Aerostructure with Integral Thermal Protection System for Kinetic Energy Interceptor

    Amount: $99,953.00

    The thermal, mechanical, and chemical environment generated during launch and flight of hypersonic missiles is severe. Ultramet has developed a melt infiltration process for rapid fabrication of refra ...

    SBIRPhase I2007Department of Defense Missile Defense Agency
  5. C/HfC Structures for Tactical Propulsion Reaction Jet Control

    Amount: $100,000.00

    Rhenium has been successfully demonstrated in solid rocket motor applications because of its high melting point and excellent strength at elevated temperatures. However, rhenium comes with a significa ...

    SBIRPhase I2007Department of Defense Air Force
  6. Passive Combustion Control Device for Noise Reduction and Improved Life in Turbine Engines

    Amount: $100,000.00

    To reduce combustion instability and noise in turbine engines, Ultramet will team with the University of Alabama to design, model, fabricate, and test refractory hafnium carbide/silicon carbide open-c ...

    SBIRPhase I2007Department of Defense Navy
  7. Economical Manufacture of Refractory Ceramic Matrix Composite Airframe with Integral Thermal Protection System

    Amount: $69,991.00

    The thermal, mechanical, and chemical environment generated during launch and flight of hypersonic projectiles is severe. Ultramet has developed a melt infiltration process for rapid fabrication of re ...

    SBIRPhase I2007Department of Defense Navy
  8. Low Temperature Gaseous Nitriding of 4340 Steel for Increased Corrosion Resistance

    Amount: $80,000.00

    Corrosion-related maintenance of metal alloy components such as hydraulic wing and blade fold actuation systems for carrier-based aircraft and rotary gear assemblies costs the Navy approximately $1 bi ...

    SBIRPhase I2007Department of Defense Navy
  9. Silicon Carbide Tritium Permeation Barriers for Steel Structural Components

    Amount: $99,996.00

    The reactor design proposed by the United States for the International Thermonuclear Experimental Reactor (ITER) requires the development of advanced materials for breeder blankets. Although recently ...

    SBIRPhase I2007Department of Energy
  10. Lightweight Ultrahigh Temperature CMC-Lined C/C Combustion Chambers, Phase II

    Amount: $600,000.00

    NASA and DoD are seeking high-performance, lightweight liquid rocket combustion chambers with future performance goals that cannot be achieved using state-of-the-art actively cooled metallic liners, s ...

    SBIRPhase II2007National Aeronautics and Space Administration
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