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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. Development of Lower Cost High Temperature Composites for Hypersonic Tactical Missiles

    Amount: $745,221.00

    The proposed Phase II effort involves 1) continued material development of low cost, high temperature composites for strategic missile components begun in Phase I, 2) the generation of an enhanced mat ...

    SBIRPhase II2007Department of Defense Air Force
  2. Development of Novel High Interlaminar Strength Carbon-Carbon Composites for Advanced Rocket Propulsion Components: Nozzle Materials and Exit Cones

    Amount: $749,994.00

    A program involving analysis and design, reinforcement materials research and development, composite fabrication, and composite property testing is proposed here to develop improved interlaminar prope ...

    SBIRPhase II2007Department of Defense Air Force
  3. Development of Low Cost Needled C/SiC for TDACS Applications

    Amount: $991,165.00

    This Phase II proposal is submitted under topic MD05-066 and continues the develop-ment of low cost, needled C/SiC for throttleable divert and altitude control systems (TDACS). The TDACS is being dev ...

    SBIRPhase II2007Department of Defense Missile Defense Agency
  4. Lightweight High Temperature Non-Eroding Throat Materials for Propulsion Systems

    Amount: $99,795.00

    The innovation in this proposed effort is the development of lightweight, non-eroding nozzle materials for use in propulsion systems. Lightweight structures are desirable for space transportation veh ...

    SBIRPhase I2007National Aeronautics and Space Administration
  5. Development of Non-Parasitic Integrated Acreage TPS/Airframe Material

    Amount: $99,915.00

    The U.S. Air Force is contemplating a long term investment in advanced thermal protection systems (TPS). The goal of this effort is to provide materials and processing solutions for TPS that can be em ...

    SBIRPhase I2006Department of Defense Air Force
  6. Development of Low Cost Needled C/SiC for TDACS Applications

    Amount: $99,862.00

    This proposal is submitted under topic MD05-066 and addresses the development of low cost, needled C/SiC for throttleable divert and altitude control systems (TDACS). The TDACS is being developed to ...

    SBIRPhase I2006Department of Defense Missile Defense Agency
  7. Evaluation of Design Concepts and Integrated Materials for Efficient Airframe Structures

    Amount: $99,963.00

    Present space vehicles such as NASA’s space shuttle and reentry bodies are designed with a cool internal structure, typically aluminum, surrounded by a parasitic thermal protection system (TPS). Th ...

    SBIRPhase I2006Department of Defense Air Force
  8. Innovative Reduced Mass TPS Designs for Human-Rated Aeroassit Vehicles

    Amount: $69,837.00

    This proposal addresses Item #2 of Topic X7.04 Aeroassist Systems and proposes innovative heat shield thermal protection systems (TPS) designs for human-rated aeroassist vehicles returning to Earth fr ...

    SBIRPhase I2006National Aeronautics and Space Administration
  9. Effects of IR Thermography-Detected Defects on Performance of SiC/SiC Composites

    Amount: $147,170.00

    In order to utilize the promising high temperature characteristics of ceramic matrix composites (CMCs) in applications such as Joint Strike Fighter (JSF) engine components, the effects of potential de ...

    SBIRPhase I2006Department of Defense Navy
  10. Novel High Strength C-C Nozzle Material for Advanced Rocket Propulsion

    Amount: $99,984.00

    MR&D proposes to develop and demonstrate lower cost versions of high temperature composites with suitable temperature ranges, which are capable of surviving the high temperature exposures of hypersoni ...

    SBIRPhase I2006Department of Defense Air Force
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