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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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Advanced Physics Modeling for Gas Turbine Particulate Ingestion
Amount: $139,994.00Ingestion of silicate particles into aircraft gas turbine (GT) engines remains a serious hazard to both commercial and military aircraft. Helicopters and low-flying fixed-wing aircraft in desert envir ...
STTRPhase I2023Department of Defense Navy -
Predict Signatures of Hypersonic Missiles
Amount: $1,499,999.00Using Combustion Research’ Flowfield Module (FM) approach, the Phase I effort laid the groundwork for the Hypersonic Vehicle Flowfield Module (HVFM) for axisymmetric/two-dimensional powered hyperson ...
SBIRPhase II2023Department of Defense Missile Defense Agency -
Landing Area and Rocket Plume Diagnostics
Amount: $149,995.00The importance of the Tactically Responsive Launch (TacRL) program lies in the fact that it increases the speed of launch operations allowing for the deployment of satellites and cargo to be made avai ...
SBIRPhase I2023Department of Defense Air Force -
Improved Hypersonic Jet Interaction Modeling with Propulsion Exhaust
Amount: $150,000.00For hypersonic glide vehicle (HGV) and hypersonic cruise missile (HCM) engagement scenarios intercept occurs in a flight regime where aerodynamic interaction and chemical reacting flow effects are lar ...
STTRPhase I2023Department of Defense Missile Defense Agency -
Predict Signatures of Hypersonic Cruise Missiles
Amount: $149,993.00Our unique position allows us to begin assessing models for hypersonic flow prediction on real-world systems and immediately begin to develop tools that will support acquisition, tracking, and traject ...
SBIRPhase I2022Department of Defense Missile Defense Agency -
A Software Toolkit to Develop OpenNCC Chemistry Models On-Demand Targeting Sustainable Aviation Fuel Blends with Soot Precursors
Amount: $149,998.00The innovation proposed is a major capability upgrade to CRAFT Techrsquo;s Multi-Time-Scale (MTS) Flamelet/Progress Variable (FPV) Software Toolkit (operational in NASArsquo;s National Combustion Code ...
SBIRPhase I2022National Aeronautics and Space Administration -
Design of Spray Cooling Systems for Chilldown of Propellant Tanks
Amount: $749,998.00In-orbit cryogenic propellant transfer is a key enabling technology for future long duration space exploration missions. Tank chilldown will be one of the primary challenges to be overcome to achieve ...
STTRPhase II2022National Aeronautics and Space Administration -
Film Condensation Modeling in Cryogenic Tank Applications
Amount: $149,997.00To support NASArsquo;s Cryogenic Fluid Management (CFM) design and operation initiatives, computational fluid dynamics (CFD) models of cryogenic condensation/liquification are required to allow for ef ...
SBIRPhase I2022National Aeronautics and Space Administration -
Multi-physics Modeling of the Ablation Process for Thermal Protection Systems
Amount: $150,000.00The goal of this effort is to develop a high-fidelity predictive capability to assess ablation response of thermal protection system (TPS) materials in extreme environments. Thermal protection syste ...
SBIRPhase I2022Department of Defense Air Force -
A Data-Efficient Software Toolkit for the Accelerated Characterization of Store Trajectories via Operator Learning
Amount: $149,997.00The innovation proposed is the development by Combustion Research and Flow Technology, Inc. (CRAFT Tech) and the University of Pennsylvania (Penn) of a software toolkit supporting the analysis of Comp ...
STTRPhase I2022Department of Defense Air Force