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COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
UEI: XGYZK5MHNJZ8
# of Employees: 24
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Autonomous UAV Aerodynamic Performance Analysis for the Near-Ship Environment
Amount: $500,000.00The overall goal of this STTR program is to develop an efficient, high-fidelity, CFD-based design tool for the simulation of ship-board flight testing of autonomous UAV systems. In the first phase of ...
STTRPhase II2014Department of Defense Navy -
Modular Flexible Weapons Integration
Amount: $149,994.00CRAFT Tech proposes the development of an innovative design optimization tool called"AeroRCS"which will simultaneously solve for both aerodynamic performance as well as electromagnetic reflectivity (R ...
SBIRPhase I2014Department of Defense Air Force -
Ceramic Matrix Composite Materials for Transpiration Cooling
Amount: $149,997.64Proposed effort will formulate and demonstrate the methodology for fabricating Porous Ceramic Matrix Composite (PCMC) transpiration plates with controlled levels of porosity, suitable for high-speed/h ...
SBIRPhase I2014Department of Defense Army -
Aerodynamic Analysis of Deployed Bay Doors on Modern High-Speed Aircraft
Amount: $743,054.00ABSTRACT: The need for evaluation of aerodynamic loads on internal weapons bay doors comes from the US Air Force's requirement to open doors on many of its aircraft during flight. This ranges from an ...
SBIRPhase II2014Department of Defense Air Force -
Physical Sub-Model Development for Turbulence Combustion Closure
Amount: $149,996.00ABSTRACT: The innovation proposed is a computationally-tractable, physics-based, portable turbulent combustion modeling strategy for application to a wide range of Air Force aero-propulsive systems, ...
STTRPhase I2014Department of Defense Air Force -
Afterburning Missile Base Flow Modeling and Analyses
Amount: $499,982.00A validated, advanced, detailed physics-based CFD capability to accurately model the separated flow physics immediately downstream in the base region of a propulsive supersonic/hypersonic missile with ...
SBIRPhase II2014Department of Defense Army -
Techniques to Suppress Cavitation in Liquid Rocket Engines
Amount: $744,777.00ABSTRACT: Next generation liquid rocket systems, envision novel designs for cryogenic turbopumps that exhibit high suction performance with low inlet pressures, operate at high tip speeds to reduce s ...
SBIRPhase II2014Department of Defense Air Force -
Design Optimization and Analysis of Advanced Exhaust Systems
Amount: $79,998.00Historically, aircraft engines have featured relatively simple axisymmetric exhaust shapes with several moving parts; however, future engine exhaust systems are expected feature compact, sinuous ducts ...
STTRPhase I2014Department of Defense Navy -
Unsteady Design Optimization for Aeroelasticity Applications
Amount: $124,997.00Aeroelasticity plays an important role in the design and development of highly flexible flight vehicles and blended wing body configurations. The operating margins on these flight systems are limited ...
SBIRPhase I2014National Aeronautics and Space Administration -
Powdered Propellant Rocket Motor
Amount: $99,999.00The preliminary design of a DAC motor using a powdered solid propellant, injected as an aerosol into the combustion chamber in a controlled manner, is formulated in this program. The injection methodo ...
SBIRPhase I2013Department of Defense Missile Defense Agency