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MATERIALS RESEARCH & DESIGN INC

Company Information
Address
300 E SWEDESFORD RD
WAYNE, PA 19087-1858
United States


https://www.m-r-d.com

Information

UEI: QU1NM7F1CDV4

# of Employees: 20


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No




Success Stories

  1. SBIR-STTR-Success: Materials Research & Design Inc.

    A small business partner has delivered a critical new tool to assist the Air Force in its race for hypersonic capabilities.With support from the Air Force Small Business Innovation Research/Small Business Technology Transfer Program, Pennsylvania-based Materials Research & Design Inc. created a...

Award Charts




Award Listing

  1. Manufacturing Process Maturation for Propulsion Technology: Structural Insulators

    Amount: $99,853.00

    MDA missile systems employ solid rocket motors and divert and attitude control systems (DACS) to propel and guide kinetic energy weapons. These systems create hot, high pressure gases that impose hig ...

    SBIRPhase I2009Department of Defense Missile Defense Agency
  2. Micromechanical Assessment of Thermochemically Induced NDE Changes in Advanced Composites

    Amount: $468,052.00

    The Joint Strike Fighter is considering the use of organic and ceramic matrix composites for high temperature engine components. Material coupons and flight tests have shown that when these materials ...

    SBIRPhase II2009Department of Defense Navy
  3. Multi-Axial Damage Index and Accumulation Model for Predicting Fatigue Life of CMC Materials

    Amount: $99,970.00

    The fatigue life of CMCs must be well characterized for the safe and reliable use of these materials as integrated TPS components. Existing fatigue life prediction models for composite materials may b ...

    SBIRPhase I2008National Aeronautics and Space Administration
  4. Thermostructural Behavior of Polymer and Ceramic Matrix Composites Under Extreme Short Term Thermal Loads

    Amount: $931,873.00

    Future supersonic missiles can be improved through the use of polymer matrix composites (PMCs) for structural airframes. However the severe aerodynamic heating conditions will expose the structure to ...

    SBIRPhase II2008Department of Defense Navy
  5. Lightweight High Temperature Non-Eroding Throat Materials for Propulsion Systems

    Amount: $599,993.00

    Radiation or passively cooled thrust chambers are used for a variety of chemical propulsion functions including apogee insertion, reaction control for launch vehicles, and primary propulsion for plane ...

    SBIRPhase II2008National Aeronautics and Space Administration
  6. Low Cost Fabrication of Carbon-Carbon (C-C) Aeroshells for Hypersonic Vehicles

    Amount: $749,869.00

    Future Air Force hypersonic vehicles will employ complex shapes and fly extended maneuvering trajectories. Since the flight times may increase by an order of magnitude or more, existing ablative ther ...

    SBIRPhase II2008Department of Defense Air Force
  7. Effects of Defects in Ceramic Matrix Composites (CMCs)

    Amount: $995,626.00

    N06-030 Effect in Defects in Ceramic Matrix Composites (CMCs) The performance of the advanced strike fighters can be im-proved by reducing the weight of the propulsion system. The jet engines of int ...

    SBIRPhase II2007Department of Defense Navy
  8. Micromechanical Assessment of Thermochemically Induced NDE Changes in Advanced Composites

    Amount: $147,261.00

    The Joint Strike Fighter is considering the use of organic and ceramic matrix composites for high temperature engine components. Material coupons and flight tests have shown that when these materials ...

    SBIRPhase I2007Department of Defense Navy
  9. Low Cost Fabrication of Carbon-Carbon (C-C) Aeroshells for Hypersonic Vehicles

    Amount: $99,941.00

    Future Air Force hypersonic vehicles will employ complex shapes and fly extended maneuvering trajectories. Since the flight times may increase by an order of magnitude or more, existing ablative ther ...

    SBIRPhase I2007Department of Defense Air Force
  10. Development of Non-Parasitic Integrated Acreage TPS/Airframe Material

    Amount: $749,498.00

    The proposed Phase II effort involves 1) continued material development of lower cost high temperature composites (PIP C/SiC) begun in Phase I, 2) modifications to the hybrid truss core integrated TPS ...

    SBIRPhase II2007Department of Defense Air Force
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