CORDEC CORP.

Company Information
Address P.O. Box 188
Lorton, VA, 22199


Information

DUNS:

# of Employees: 6


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  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 ...

    SBIRPhase I1998Army Department 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 ...

    SBIRPhase I1997Army Department of Defense
  3. Laser Consolidation of Silicon Carbide/Titanium Metal Composite Turbine Rings

    Amount: $75,000.00

    N/A

    SBIRPhase I1995Department 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 ...

    SBIRPhase I1994Air Force Department of Defense
  5. 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 ...

    SBIRPhase I1993Missile Defense Agency Department of Defense
  6. 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 ...

    SBIRPhase I1993Army Department of Defense
  7. Vapor Deposited, Metal-Matrix Composites for Dimensional Stability without Hysteresis

    Amount: $49,996.00

    N/A

    SBIRPhase I1993National Aeronautics and Space Administration
  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 ...

    SBIRPhase I1990National 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 ...

    SBIRPhase I1990National 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 ...

    SBIRPhase I1990Navy Department of Defense

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