MATERIALS RESEARCH & DESIGN INC

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

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

Information

DUNS: 966563884

# of Employees: 20


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Mechanism Based Damage Model for Linerless Thin-Ply Composite Pressure Vessels

    Amount: $124,510.00

    Thin-ply composites are being considered by NASA for space exploration applications, where the suppression of microcracks could give rise to linerless cryogenic tanks. In this proposed Phase I STTR e ...

    STTRPhase I2017National Aeronautics and Space Administration
  2. A Mathematical Model to Assess CMAS Damage in EBCs

    Amount: $124,930.00

    As the power density of advanced engines increases, the need for new materials that are capable of higher operating temperatures, such as ceramic matrix composites (CMCs), is critical for turbine hot- ...

    SBIRPhase I2017National Aeronautics and Space Administration
  3. Load Bearing Thermal Protection Structure for Hypersonic Flight

    Amount: $149,276.56

    The proposed effort will investigate three types of structurally-integrated thermal protection system (SITPS) concepts that can be readily manufactured, and which have shown promising performance in p ...

    SBIRPhase I2017Department of Defense Defense Advanced Research Projects Agency
  4. Rayon Replacement for High Temperature Materials

    Amount: $99,991.00

    Materials Research & Design, Inc. (MR&D) proposes program to demonstrate repeatable processability of low conductivity, low modulus, high strength, Lyocell based materials that can provide sustained, ...

    SBIRPhase I2017Department of Defense Missile Defense Agency
  5. Ceramic-Metal Joining for Hypersonic Vehicle and Missile Components

    Amount: $499,961.00

    Advanced Navy systems such as the Hyper Velocity Projectile (HVP) and next generation high speed missiles will subject the airframe to severe aerothermal heating loads. Both the HVP fin and missile ra ...

    SBIRPhase II2017Department of Defense Navy
  6. Generating Material Properties From Flight Representative Structures

    Amount: $149,782.45

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

    STTRPhase I2017Department of Defense Defense Advanced Research Projects Agency
  7. Evaluation of Alternative Carbon Fibers to Improve Joint Performance in 3D Woven Heatshields

    Amount: $124,998.00

    Abstract

    SBIRPhase I2016National Aeronautics and Space Administration
  8. Fiber Optic Health Monitoring of 3D Woven Preforms and Composites Employing Structurally Integrated Sensors

    Amount: $124,593.00

    Woven TPS (WTPS) is an attractive option for thermal protection because it allows for a design to be tailored to a specific mission ? material composition can be adjusted by weaving different fiber ty ...

    STTRPhase I2016National Aeronautics and Space Administration
  9. Ceramic Matrix Composite Environmental Barrier Coating Durability Model

    Amount: $749,880.00

    As the power density of advanced engines increases, the need for new materials that are capable of higher operating temperatures, such as ceramic matrix composites (CMCs), is critical for turbine hot- ...

    STTRPhase II2016National Aeronautics and Space Administration
  10. Ceramic-Metal Joining for Hypersonic Vehicle and Missile Components

    Amount: $79,936.00

    Advanced Navy systems such as the Hyper Velocity Projectile (HVP) and next generation high speed missiles will subject the airframe to severe aerothermal heating loads. Both the HVP fin and missile ra ...

    SBIRPhase I2016Department of Defense Navy

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