DWA ALUMINUM COMPOSITES

Address

21100 Superior St.
Chatsworth, CA, -

Information

DUNS: 75293233
# of Employees: 17

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  1. SiCp/Al MMC Bearing Liners

    Amount: $79,848.00

    DWA Aluminum Composites proposes the use of powder-metallurgy based, silicon carbide particulate (SiCp) reinforced aluminum Metal-Matrix-Composites (MMCs) for the replacement of 4320 steel alloy beari ...

    SBIRPhase I2011Department of Defense
  2. Cost-Effective Manufacturing for L12 Strengthened Aluminum Alloys

    Amount: $99,927.00

    The use of aluminum in rocket engine turbo-machinery has not been realized due to strength limitations at elevated temperature. This Phase I SBIR proposal addresses innovative, cost-effective manufac ...

    SBIRPhase I2003Department of Defense
  3. Affordable Nanophase Aluminum for Launch Vehicle Propulsion

    Amount: $99,944.00

    N/A

    SBIRPhase I1999Air Force Department of Defense
  4. Deformation Process Modeling of DRA Extrusions

    Amount: $99,946.00

    The lack of fully developed extrusion design tools for Discontinuously Reinforced Aluminum (DRA) such as finite element simulation codes will continue to impede market penetration of this promising ae ...

    SBIRPhase I1998Air Force Department of Defense
  5. DEMONSTRATION OF LOW CTE PARTICULATE REINFORCED METAL MATRIXCOMPOSITE MATERIAL

    Amount: $500,000.00

    CURRENT SPACE STRUCTURE JOINTS AND COUPLINGS REQUIRE LOW CTE WHILE MAINTAINING LIGHTWEIGHT AND STRUCTURAL INTEGRITY. THEY MUST ALSO BE FABRICABLE AND OF AFFORDABLE COST. NO MATERIAL DEVELOPED TO DATE ...

    SBIRPhase II1989National Aeronautics and Space Administration
  6. HIGH SPECIFIC STRENGTH/STIFFNESS METAL MATRIX COMPOSITE TORPEDO HULL SECTIONS

    Amount: $49,979.00

    THIS PHASE I EFFORT WILL SHOW THE FEASIBILITY OF THE FABRICATION OF HIGH SPECIFIC STRENGTH/STIFFNESS, B(4)C REINFORCED ALUMINUM METAL MATRIX COMPOSITE (MMC) TORPEDO HULLS. CURRENT TORPEDO HULLS ARE CO ...

    SBIRPhase I1989Navy Department of Defense
  7. DEVELOPMENT OF PLANAR ISOTROPIC NEAR ZERO CTE GR/AL SPHERICAL REFLECTORS

    Amount: $49,974.00

    CURRENT ANTENNA REFLECTORS ARE PRIMARILY MADE FROM GR/EPOXY OR CARBON-CARBON COMPOSITES, AND THESE MATERIAL SYSTEMS OFFER LIMITATIONS IN SURVIVABILITY AND MECHANICAL PROPERTIES. THESE LIMITATATIONS CO ...

    SBIRPhase I1988Navy Department of Defense
  8. DEMONSTRATION OF LOW CTE PARTICULATE REINFORCED METAL MATRIXCOMPOSITE MATERIAL

    Amount: $49,954.00

    N/A

    SBIRPhase I1988National Aeronautics and Space Administration
  9. TUBULAR COMPOSITE STRUCTURAL ELEMENTS WITH INTEGRAL END FITTINGS

    Amount: $229,000.00

    COUPLING HIGH-PERFORMANCE METAL-MATRIX COMPOSITE STRUCTURAL ELEMENTS WITH END FITTINGS OF COMPARABLE HIGH PERFORMANCE PROMISES THE CAPABILITY OF FABRICATING STRUCTURES OF EXCEPTIONAL STRENGTH, RIGIDIT ...

    SBIRPhase II1987National Aeronautics and Space Administration
  10. COMPOSITE HEAT PIPE CONCEPTS USING PITCH GRAPHITE/METAL CPMPOSISTES

    Amount: $125,000.00

    FEASIBILITY WILL BE DEMONSTRATED FOR USE OF HIGH STIFFNESS HIGH THERMAL CONDUCTIVITY PITCH GRAPHIC REINFORCED-METAL COMPOSITES IN SIMPLE HEAT-PIPE CONCEPTS. THE VERY HIGHLY ANISOTROPIC THERMAL CONDUCT ...

    SBIRPhase II1987National Aeronautics and Space Administration

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