Materials Research & Design

Basic Information

300 E. Swedesford Rd
Wayne, PA, -

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

Company Profile

n/a

Additional Details

Field Value
DUNS: 966563884
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 23


  1. Innovative Interlaminar Mode I and Mode II Fracture Toughness Test Methods for Ceramic Matrix Composites

    Amount: $749,954.00

    It is critical to the safe use of ceramic matrix composite components that information on the fracture toughness of these materials be available in order to allow an assessment of the likelihood for c ...

    STTR Phase II 2015 Department of DefenseNavyDepartment of Defense
  2. Process Optimization of Needled Carbon/ silica carbide (C/SiC) Structural Insulators

    Amount: $999,960.00

    Some missiles employ a throttleable divert and altitude control system (TDACS) to maneuver the kill vehicle to the target. Hot gas valve components in the TDACS must survive long burn times at high p ...

    SBIR Phase II 2015 Department of DefenseMissile Defense AgencyDepartment of Defense
  3. Improved Materials and Designs for High Pressure Wind Tunnel Applications

    Amount: $149,922.00

    ABSTRACT: This Phase I effort will identify and evaluate candidate materials to replace existing beryllium-copper alloy components for use in aerospace ground test flow facilities. The candidate mate ...

    STTR Phase I 2015 Department of DefenseAir ForceDepartment of Defense
  4. Investigation of Effect of High, Short Duration Temperatures on Fiber Graphitization and Resulting Property Changes in 3D Woven TPS Preforms During Entry Trajectories

    Amount: $124,937.00

    To address the need for low-ballistic coefficient aeroshells with minimal impact on vehicle weight, NASA is investigating flexible thermal protection system (TPS) options. These designs typically cons ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  5. Ceramic Matrix Composite Environmental Barrier Coating Durability Model

    Amount: $118,914.00

    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- ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  6. Fine Braided Tungsten Reinforced Ceramic Composites for Ultra Sharp Structures

    Amount: $79,451.00

    Future hypersonic vehicles will be required to fly extended, long term trajectories where the bod-ies must exhibit high lift-to-drag (L/D) ratios. The need for reduced drag means that the nosetips and ...

    SBIR Phase I 2014 Department of DefenseNavyDepartment of Defense
  7. Integrated Lighning Strike and Electromagnetic Interference (EMI) Protection Thermal Protection System (TPS) Materials for Missile Skin Structures

    Amount: $124,989.00

    Lightning protection is crucial for atmospheric flight of any missile vehicle. The direct and indirect effects of lightning can easily cause catastrophic failure of a missile due to structural breach ...

    SBIR Phase I 2014 Department of DefenseMissile Defense AgencyDepartment of Defense
  8. Nonlinear Material Models for Design of Carbon-Carbon Composites

    Amount: $79,990.00

    Advanced Navy reentry vehicles will use 2D and 3D carbon-carbon (CC) thermal protection system (TPS) components in order to survive conditions imposed by high speed flight. The TPS structures are expo ...

    SBIR Phase I 2014 NavyDepartment of DefenseDepartment of Defense
  9. Manufacturing Process Maturation for Propulsion Technology: Structural Insulators

    Amount: $1,106,014.00

    ABSTRACT: The Arnold Engineering Development Complex (AEDC) represents the nation"s largest aerospace ground test facilities and includes several wind tunnels that are unlike any other in the wo ...

    SBIR Phase II 2014 Air ForceDepartment of DefenseDepartment of Defense
  10. Calculation of Effective Material Strengths for 3D Woven Hybrid Preforms and Composites

    Amount: $749,525.00

    The design concepts being considered for Heatshield for Extreme Entry Environment Technology (HEEET) rely on the use of 3D woven carbon fiber preforms. Therefore, there is a need to be able to predic ...

    SBIR Phase II 2014 National Aeronautics and Space Administration

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