DWA ALUMINUM COMPOSITES

Basic Information

21100 Superior St.
Chatsworth, CA, -

Company Profile

n/a

Additional Details

Field Value
DUNS: 75293233
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 17


  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 ...

    SBIR Phase I 2011 Department of Defense Navy
  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 ...

    SBIR Phase I 2003 Department of Defense Air Force
  3. Affordable Nanophase Aluminum for Launch Vehicle Propulsion

    Amount: $99,944.00

    N/A

    SBIR Phase I 1999 Air 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 ...

    SBIR Phase I 1998 Air 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 ...

    SBIR Phase II 1989 National 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 ...

    SBIR Phase I 1989 Navy 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 ...

    SBIR Phase I 1988 Navy Department of Defense
  8. DEMONSTRATION OF LOW CTE PARTICULATE REINFORCED METAL MATRIXCOMPOSITE MATERIAL

    Amount: $49,954.00

    N/A

    SBIR Phase I 1988 National 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 ...

    SBIR Phase II 1987 National 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 ...

    SBIR Phase II 1987 National Aeronautics and Space Administration

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