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COMBUSTION RESEARCH AND FLOW TECHNOLOGY INC

Company Information
Address
6210 KELLERS CHURCH RD
PIPERSVILLE, PA 18947-1020
United States


http://www.craft-tech.com

Information

DUNS: 929950012

# of Employees: 32


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Physical Sub-Model Development for Turbulence Combustion Closure

    Amount: $149,996.00

    ABSTRACT: 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
  2. Afterburning Missile Base Flow Modeling and Analyses

    Amount: $499,982.00

    A 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
  3. Techniques to Suppress Cavitation in Liquid Rocket Engines

    Amount: $744,777.00

    ABSTRACT: 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
  4. Design Optimization and Analysis of Advanced Exhaust Systems

    Amount: $79,998.00

    Historically, 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
  5. Unsteady Design Optimization for Aeroelasticity Applications

    Amount: $124,997.00

    Aeroelasticity 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
  6. Powdered Propellant Rocket Motor

    Amount: $99,999.00

    The 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
  7. Design Combined Effects Explosives (CEX) Using Numerical Simulations

    Amount: $149,987.00

    Combustion Research and Flow Technology, Inc. (CRAFT Tech) and Prof. Glumac of the University of Illinois at Urbana-Champaign (UIUC) have teamed up to provide DTRA with an innovative approach to devel ...

    SBIRPhase I2013Department of Defense Defense Threat Reduction Agency
  8. Short Duration, High Altitude, Mixed Continuum/Non-Continuum Flowfield

    Amount: $99,998.00

    The problem to be addressed within the present proposal is the accurate modeling of high altitude transient phenomena associated with short duration propulsive and/or detonative events taking into acc ...

    SBIRPhase I2013Department of Defense Army
  9. Afterburning Missile Base Flow Modeling and Analyses

    Amount: $99,998.00

    Finite-rate turbulence- chemistry interaction methodology will be implemented in the CRAFT CFD code to improve high-speed afterburning base flow predictions. UMiss/NCPA will conduct hot-rocket model t ...

    SBIRPhase I2013Department of Defense Army
  10. Characterization and Incorporation of Vernier Engines within the Plume Modeling Process

    Amount: $1,499,993.00

    Plume signature phenomenology plays an increasingly important role in the development of a wide variety of missile defense technologies, both at the tactical and strategic levels. With the emergence o ...

    SBIRPhase II2013Department of Defense Missile Defense Agency
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