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MATERIALS RESEARCH & DESIGN INC
UEI: QU1NM7F1CDV4
# of Employees: 20
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Thermostructural Behavior of Polymer and Ceramic Matrix Composites Under Extreme Short Term Thermal Loads
Amount: $99,858.00Future supersonic missiles can be improved through the use of PMCs and CMCs for structural airframes. However the severe aerodynamic heating conditions that the missiles undergo will expose the struc ...
SBIRPhase I2006Department of Defense Navy -
Development of Lower Cost High Temperature Composites for Hypersonic Tactical Missiles
Amount: $99,984.00MR&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 -
Design and Life Prediction Methodologies for Weight Efficient Ceramic Matrix Composite (CMC) Propulsion Components
Amount: $1,764,380.00The performance of the JSF can be improved by reducing the weight of the propulsion system. The JSF is powered by either Pratt & Whitney’s (P&W) F135 engine or General Electric’s F136 engine. Bo ...
SBIRPhase II2005Department of Defense Navy -
Innovative 2D Ceramic Matrix Composites for Improved Interlaminar Strengths
Amount: $79,664.00The performance of the JSF can be improved through the use of CMCs because they offer lower weight, improved high temperature strengths, and better performance than existing metal components. Recent ...
SBIRPhase I2005Department of Defense Navy -
Innovative Manufacturing Process Improvements: HIP Process Model
Amount: $99,995.00The Missile Defense Agency (MDA) and other components of the Department of Defense (DOD) are cur-rently developing advanced materials for propulsion hardware, weapons systems, thermal management appli ...
SBIRPhase I2005Department of Defense Missile Defense Agency -
PROPULSION MATERIALS MODELING TO IMPROVE PERFORMANCE AND REDUCE COST
Amount: $99,939.00MDA is developing materials for several applications including hypersonic missiles, ma-neuvering reentry vehicles, advanced solid rocket motors, and divert and attitude control sys-tems. All of these ...
STTRPhase I2005Department of Defense Missile Defense Agency -
Design Concepts for CMC Leading Edges with Embedded Metallic Heat Pipes
Amount: $99,964.00This effort explores and assesses the options available for refractory composite leading edges cooled by embedded metallic heat pipes. Currently, the heat pipe cooled leading edges (HPCLE's) being in ...
SBIRPhase I2005Department of Defense Air Force -
Optimized Hybrid Leading Edge for Reusable Launch Vehicles to Maximize Lift, Cross Range and Durability
Amount: $99,973.00This effort explores using innovative hybrid reinforced carbon-carbon, refractory ceramics, super alloys and composite materials as thermal protection system (TPS) in Hybrid composite leading edges fo ...
SBIRPhase I2004Department of Defense Air Force -
Investigation of Non Eroding Nozzle Materials for Optimized Coated Hybrid Leading Edge Designs For Reusable Launch Vehicals With Leading Edge Radii of 0.03? TO 1? and Temperatures Near 4000?F
Amount: $69,658.00Effort explores using innovative hybrid reinforced carbon-carbon, refractory ceramics, super alloys and composite materials as thermal protection system specifically in the 4000?F range with leading e ...
SBIRPhase I2004National Aeronautics and Space Administration -
Design and Life Prediction Methodologies for Weight Efficient Ceramic Matrix Composite (CMC) Propulsion Components
Amount: $99,994.00Ceramic matrix composites (CMCs) are being developed for the exhaust nozzle of the Joint Strike Fighter (JSF) because they offer significant weight reduction and high temperature capability. The use ...
SBIRPhase I2004Department of Defense Navy