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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. Analytical Design of Surface Porosity in 2D C/C to Delay Boundary Layer Transition for Hypersonic Aeroshell Applications

    Amount: $139,698.00

    Materials Research & Design, Inc. (MR&D) is proposing a combined experimental and analytical effort to develop a method for introducing a specified surface porosity that is capable of stabilizing the ...

    SBIRPhase I2019Department of Defense Navy
  2. Unit-Cell Approach for C/C Process and Mechanical Modeling

    Amount: $149,594.00

    The properties of carbon-carbon composites often exhibit significant variability due to variations in processing conditions and spatial variations inherent in the material structure of fabric-reinforc ...

    SBIRPhase I2019Department of Defense Air Force
  3. A User Element (UEL) Based Process Model for Prediction of Carbon-Carbon Dimensional Changes During Manufacturing

    Amount: $149,950.00

    The process of manufacturing structural carbon-carbon composites is one fraught with variability. Many of the standard practices employed by fabricators have, in some way, been derived from both exper ...

    SBIRPhase I2019Department of Defense Air Force
  4. A User Element (UEL) Based Process Model for Prediction of Carbon-Carbon Dimensional Changes During Manufacturing

    Amount: $149,991.00

    The process of manufacturing phenolic-derived structural carbon-carbon composites is one fraught with variability. Many of the standard practices employed by fabricators have, in some way, been derive ...

    SBIRPhase I2019Department of Defense Air Force
  5. Melt-Infiltrated Carbon-Carbon Nosetips and Leading Edges for High Velocity, Gun-Launched Projectiles

    Amount: $224,936.00

    Recently developed high velocity projectiles employ tungsten nosetips and titanium alloy control surfaces. The tungsten nose remains thermochemically stable at current muzzle velocities and provides b ...

    SBIRPhase I2019Department of Defense Office of the Secretary of Defense
  6. Uncertainty Reduction in High Speed Flight Vehicle Modeling

    Amount: $99,670.00

    Uncertainty Reduction in High Speed Flight Vehicle Modeling | Approved for Public Release 18-MDA-9707 (3 Jul 18)

    STTRPhase I2019Department of Defense Missile Defense Agency
  7. Tape-Wrapped Carbon / Silicon Carbide Composites for Launch Vehicle Applications

    Amount: $149,864.00

    To ensure continued access to orbit for United States government and commercial payloads, attractive replacement candidates for foreign-made propulsion components must be identified and the associated ...

    SBIRPhase I2018Department of Defense Air Force
  8. Development of Lyocell-Based High Temperature Composites for Structural Insulator Applications

    Amount: $998,111.00

    Materials Research & Design, Inc. submits this Phase II SBIR proposal to address Rayon Replacement for High Temperature Materials. The proposed program seek to demonstrate repeatable processability of ...

    SBIRPhase II2018Department of Defense Missile Defense Agency
  9. Thin-Ply Composite Missile Structures

    Amount: $99,980.00

    The Missile Defense Agency (MDA) has multiple system platforms to defeat an Intercontinental Ballistic Missile (ICBM).The MDAs solution for defeating a midcourse threat is the Ground-Based Midcourse I ...

    STTRPhase I2018Department of Defense Missile Defense Agency
  10. Generating Material Properties From Flight Representative Structures

    Amount: $1,498,880.00

    High-speed flight vehicles commonly use carbon / carbon (C/C) and carbon / silicon carbide (C/SiC) for structural components. These materials are chosen because of their superior structural properties ...

    STTRPhase II2018Department of Defense Defense Advanced Research Projects Agency
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