DWA ALUMINUM COMPOSITES

Company Information

Company Name
DWA ALUMINUM COMPOSITES
Address
21100 Superior St.
Chatsworth, CA, -
Phone
1 818-998-1504
URL
n/a
DUNS
75293233
Number of Employees
17
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$1,224,831.00
21
SBIR Phase II
$3,260,309.00
9

Award List

  1. HIGH-TEMPERATURE METAL-MATRIX STRUCTURE

    Amount: $313,410.00

    THIS PHASE I PROGRAM PROPOSES FIRST TO DEMONOSTRATE THE FEASIBILITY OF PRODUCING A CERAMIC PARTICULATE-REINFORCED SUPERALLOY MMC, AND SECONDLY TO SHOW THAT THE NEW MATERIAL CAN FUNCTION USEFULLY FOR S ...

    SBIR Phase II 1985 Air ForceDepartment of Defense
  2. A UNIQUE ALUMINUM BRONZE MATRIX COMPOSITE HAS BEEN DEVELOPED THAT OFFERS ATTRACTIVE PROPERTIES FOR ELEVATED-TEMPERATURE USE.

    Amount: $48,480.00

    A UNIQUE ALUMINUM BRONZE MATRIX COMPOSITE HAS BEEN DEVELOPED THAT OFFERS ATTRACTIVE PROPERTIES FOR ELEVATED-TEMPERATURE USE. THIS PHASE I PROGRAM WILL FABRICATE EXTRUDED ALUMINUM-BRONZE MATRIX COMPOSI ...

    SBIR Phase I 1984 National Aeronautics and Space Administration
  3. ELECTRONIC COMPONENT TEMPERATURE CONTROL USING METAL-MATRIX COMPOSITES

    Amount: $471,669.00

    THIS PHASE I PROGRAM IS INTENDED TO DEMONSTRATE THE FEASIBILITY OF PRODUCING A LIGHTWEIGHT METAL-MATRIX COMPOSITE (MMC) HEAT-REMOVAL BAR HAVING THE THERMAL CONDUCTIVITY OF COPPER AND TO SHOW, BY MECHA ...

    SBIR Phase II 1986 National Aeronautics and Space Administration
  4. LOW CTE METAL MATRIX COMPOSITE FITTINGS

    Amount: $498,230.00

    THIS PHASE I PROGRAM IS DESIGNED TO DEMONSTRATE THE FEASIBILITY OF PRODUCING LIGHTWEIGHT, LOW CTE METAL-MATRIX COMPOSITE FITTINGS OF GRAPHITE-FIBER/ALUMINUM AND TO SHOW BY MECHANICAL AND PHYSICAL-PROP ...

    SBIR Phase II 1986 National Aeronautics and Space Administration
  5. 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
  6. 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
  7. MOST SPACECRAFT, PARTICULARLY MANNED VEHICLES, HAVE DIVERSIFIED POWER REQUIREMENTS NECESSITATING A VARIETY OF THERMAL-CONTROL CAPABILITEIS FOR BOTH PRIMARY SYSTEMS AND CONTINGENCY OPERATIONS.

    Amount: $49,854.00

    MOST SPACECRAFT, PARTICULARLY MANNED VEHICLES, HAVE DIVERSIFIED POWER REQUIREMENTS NECESSITATING A VARIETY OF THERMAL-CONTROL CAPABILITEIS FOR BOTH PRIMARY SYSTEMS AND CONTINGENCY OPERATIONS. TO ACCOM ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  8. END FITTINGS FOR HINGED AND RIGID JINTS BETWEEN GRAPHITE-ALUMINUM TUBULAR STRUCTURAL ELEMENTS

    Amount: $125,000.00

    BY ATTACHING (VIA WELDING OR BONDING) ARTICULATED TERMINATORS ONTO HIGH-PERFORMANCE GRAPHITE-ALUMINUM TUBULAR STRUCTURAL ELEMENTS, HINGED ANDD RIGID JINTS CAN BE STABLE DWA1 20 METAL-MATRIX COMPOSITES ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
  9. EXPLORING THE FEASIBILITY OF COMBINING MATERIALS TO PRODUCE HIGH SPECIFIC MODULUS AND STRENGTH IN A SINGLE COMPOSITE

    Amount: $499,000.00

    GRAPHITE FIBER IS ONE OF THE MOST VERSATILE REINFORCEMENTS KNOWN. WITH PAN BASED PRECURSOR, TENSILE STRENGTHS UP TO 1.2 MSI WILL BE AVAILABLE IN FY1986 AND WITH PITCH BASED PRECURSOR, MODULUS OF ELAST ...

    SBIR Phase II 1987 NavyDepartment of Defense
  10. HYBRID MMC MATERIALS FOR JOINING OF THERMALLY MIS-MATCHED MISSILE COMPONENTS DEVELOPMENT

    Amount: $499,000.00

    THIS PHASE I PROGRAM WILL DEMONSTRATE THE ABILITY OF UTILIZING HYBRID METAL-MATRIX COMPOSITES (MMC) ON SELECTED NAVY MISSILE STRUCTURES WHERE TWO STRUCTURES, OR SUBELEMENTS OF MARKEDLY DIFFERENT C.T.E ...

    SBIR Phase II 1987 NavyDepartment of Defense

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