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RESEARCH APPLICATIONS, INC.
UEI: N/A
# of Employees: 4
HUBZone Owned: Yes
Socially and Economically Disadvantaged: Yes
Woman Owned: No
Award Charts
Award Listing
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Coated Ceramic Matrix Composite (CMC) Low Pressure Turbine (LPT) Blade Development
Amount: $99,738.00The objective of this Phase I SBIR is to assess feasibility of developing, validating and marketing a methodology and software for timely and cost effective implementation of advanced Ceramic Matrix C ...
SBIRPhase I2009Department of Defense Air Force -
Three-Dimensional Deformation and Life Prediction Methods for Ceramic Matrix Composite Components
Amount: $747,913.00Innovative research and development leading to a dual-use advanced technology product is proposed. The product is a methodology and associated software for three-dimensional design and life prediction ...
SBIRPhase II2007Department of Defense Air Force -
Three-Dimensional Deformation and Life Prediction Methods for Ceramic Matrix Composite Components
Amount: $99,416.00Innovative research and development leading to a dual-use advanced technology product is proposed. The product is a methodology and associated software for three-dimensional design and life predictio ...
SBIRPhase I2006Department of Defense Air Force -
Methodology for Modeling Based Assessment of TPS Concepts
Amount: $749,626.00Innovative research and development leading to a dual-use advanced technology product is proposed. The product is a methodology and associated software for design and life prediction of ceramic matri ...
SBIRPhase II2005Department of Defense Air Force -
Improved Models for Coated CMC Components with Severe Thermal Gradients
Amount: $729,281.00The present proposal is aimed at developing a commercially marketable product in the form of a computer-based methodology and software tools for design and life prediction of ceramic matrix composite ...
SBIRPhase II2005Department of Defense Army -
Thermal Barrier Coating Life Determination
Amount: $99,932.00The goal is to develop and experimentally validate a marketable methodology for remaining life evaluation of thermal barrier coated (TBCed) turbine engine components using quantitative nondestructive ...
SBIRPhase I2005Department of Defense Air Force -
Improved Models for Coated CMC Components with Severe Thermal Gradients
Amount: $119,849.00Innovative research and development leading to a dual-use advanced technology product is proposed. The product is a methodology and associated software for design and life prediction of ceramic matri ...
SBIRPhase I2005Department of Defense Army -
Design Tools for Fatigue Life Prediction in Surface Treated Aerospace Components
Amount: $79,727.00A methodology and software for life prediction of surface treated components is sought to complement existing life prediction technology. An innovative approach with high probability of success is pr ...
SBIRPhase I2005Department of Defense Navy -
Innovative Weight Efficient Combined Structural/Thermal Protection System (TPS) Concepts
Amount: $99,517.00Innovative research and development leading to a dual-use advanced technology product is proposed. The product is a methodology and associated software for design and life prediction of ceramic matri ...
SBIRPhase I2004Department of Defense Air Force -
Defect and Damage Assessment Methodology for CMC Components
Amount: $79,273.00Innovative research and development leading to a dual-use advanced technology product is proposed. The product is a methodology and associated software for defect and damage assessment of ceramic mat ...
SBIRPhase I2004Department of Defense Navy