You are here
MATERIALS RESEARCH & DESIGN INC
UEI: QU1NM7F1CDV4
# of Employees: 20
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
-
Calculation of Effective Material Strengths for 3D Woven Hybrid Preforms and Composites
Amount: $749,525.00The 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 ...
SBIRPhase II2014National Aeronautics and Space Administration -
Improved Foreign Object Damage Performance for 3D Woven Ceramic Matrix Composites
Amount: $749,362.00As 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 II2014National Aeronautics and Space Administration -
Calculation of Effective Material Strengths for 3D Woven Hybrid Preforms and Composites
Amount: $124,761.00Current NASA programs, such as Adaptable, Deployable Entry and Placement Technology (ADEPT) and Woven Thermal Protection Systems (WTPS) are looking to fill a gap in ablative TPS for future missions to ...
SBIRPhase I2013National Aeronautics and Space Administration -
Test Methods for the Determination of Anisotropic Compliances in 3D Woven Preforms for Ablative TPS
Amount: $124,995.00Based on the recent success of the Mars Exploration Program and the Mars Science Laboratory mission, NASA has a desire to expand on the technology developed under each effort in order to increase futu ...
SBIRPhase I2013National Aeronautics and Space Administration -
Improved Foreign Object Damage Performance for 2D Woven Ceramic Matrix Composites
Amount: $124,842.00As 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 I2013National Aeronautics and Space Administration -
Innovative Nosetip Materials and Designs for Hypervelocity Projectiles
Amount: $79,913.00The Navy is developing high speed projectiles for a variety of missions including ship defense, surface fire support, and prompt global strike. Inertial loads and high muzzle velocities impose severe ...
SBIRPhase I2013Department of Defense Navy -
Innovative Interlaminar Mode I and Mode II Fracture Toughness Test Methods for Ceramic Matrix Composites
Amount: $79,985.00It 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 ...
STTRPhase I2013Department of Defense Navy -
Lightweight Composite/Hybrid Structures with Enhanced Properties
Amount: $99,972.00ABSTRACT: Future hypersonic vehicles, like X-43 and X-51 derivatives and Falcon HTV-3, will require advanced strategies for thermal protection systems (TPS) and methods of structural integration. Th ...
STTRPhase I2012Department of Defense Air Force -
Alternative Fabrication Designs for Carbon-Carbon (C-C) Nozzle Extensions
Amount: $124,989.00In order for carbon-carbon nozzle extensions and exit cones to serve as practical, low cost components for future Earth-to-Orbit propulsion systems, it is necessary to develop alternative fabrication ...
SBIRPhase I2012National Aeronautics and Space Administration -
Low-Erosion and Affordable Nozzles for Advanced Air-to-Air Missiles
Amount: $79,997.00One of the main drivers in the design of nozzles for advanced air-to-air missiles deals with erosion caused by combustion gases. Erosion can happen by melting/sublimation, oxidation and mechanical abr ...
SBIRPhase I2012Department of Defense Navy