CORDEC CORP.

Basic Information

P.O. Box 188
Lorton, VA, 22199

Company Profile

n/a

Additional Details

Field Value
DUNS: n/a
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 6


  1. Rapid Consolidation of Near Net Shape Titanium Alloy Composites for Helicopter Turbines

    Amount: $99,776.00

    The extraordinary potential of high-temperature composite materials to meet the engineering design challenges presented by advanced turbine engines is well known. Implementation has been seriously im ...

    SBIR Phase I 1998 ArmyDepartment of DefenseDepartment of Defense
  2. Microstructurally Tailored High Temperature Metal Matrix Composites for Advanced Turbines

    Amount: $96,741.00

    Successful development of advanced turbine engines will depend heavily upon rapid development of new, reliable, lightweight metal matrix composites (MMC's) having unprecedented high temperature proper ...

    SBIR Phase I 1997 ArmyDepartment of DefenseDepartment of Defense
  3. Laser Consolidation of Silicon Carbide/Titanium Metal Composite Turbine Rings

    Amount: $75,000.00

    N/A

    SBIR Phase I 1995 Department of Energy
  4. Self-Aligning Composite Monotapes for Homogeneous Reinforcement of High Temperature Metal Matrix Composites

    Amount: $79,902.00

    The extraordinary potential of high-temperature composite materials to meet the engineering design challenges presented by advanced turbine engines and hypersonic flight vehicle airframes is well know ...

    SBIR Phase I 1994 Air ForceDepartment of DefenseDepartment of Defense
  5. Vapor Deposited, Metal-Matrix Composites for Dimensional Stability without Hysteresis

    Amount: $49,996.00

    N/A

    SBIR Phase I 1993 National Aeronautics and Space Administration
  6. Advanced Intermetallic Matrix Composites

    Amount: $49,525.00

    MANY CURRENT AND PLANNED DEFENSE AEROSPACE PROGRAMS DEPEND CRITICALLY UPON RAPID DEVELOPMENT OF LIGHTWEIGHT COMPOSITE MATERIALS HAVING UNPRECEDENTED HIGH-TEMPERATURE PROPERTIES. CONTINUOUS FIBER REINF ...

    SBIR Phase I 1993 Missile Defense AgencyDepartment of DefenseDepartment of Defense
  7. Fabrication of High Temperature Metal Matrix Composite Tubes by Vapor Deposition Methods

    Amount: $49,985.00

    Advanced turbine engines and flight vehicles will depend upon new, high-temperature metal matrix composites (MMC's) to meet performance goals. Engineering characterization of such materials is difficu ...

    SBIR Phase I 1993 ArmyDepartment of DefenseDepartment of Defense
  8. NEW FABRICATION METHODS FOR DIMENSIONALLY STABLE GRAPHITE/MAGNESIUM SPACE STRUCTURES

    Amount: $49,953.00

    OUR RECENT EFFORTS IN FABRICATING THIN-GAUGE GRAPHITE/MAGNESIUM COMPOSITES HAVE RESULTED IN THE FIRST SUCH MATERIAL TO HAVE A ZERO COEFFICIENT OF THERMAL EXPANSION AND NO PERCEPTIBLE DIMENSIONAL HYSTE ...

    SBIR Phase I 1990 National Aeronautics and Space Administration
  9. MICROSTRUCTURALLY TOUGHENED INTERMETALLIC MATRIX COMPOSITES

    Amount: $49,880.00

    SUCCESSFUL DEVELOPMENT OF HYPERSONIC FLIGHT VEHICLES AND ENGINES WILL DEPEND HEAVILY UPON RAPID DEVELOPMENT OF NEW, HIGH-TEMPERATURE METAL MATRIX COMPOSITE (MMC'S). FIBER REINFORCED TITANIUM ALUMINIDE ...

    SBIR Phase I 1990 National Aeronautics and Space Administration
  10. FUNCTIONALLY GRADIENT ELECTRONIC HEAT SINK MATERIALS

    Amount: $49,963.00

    RELIABILITY AND CIRCUIT DENSITY OF STANDARD ELECTRONIC MODULES (SEM) CAN BE INCREASED SIGNIFICANTLY BY TAILORING THERMOPHYSICAL PROPERTIES OF THE HEAT SINK MATERIALS. NEWLY DEVELOPED TECHNIQUES FOR MA ...

    SBIR Phase I 1990 NavyDepartment of DefenseDepartment of Defense

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