Tetra Research Corporation

Company Information
Address 629 Park Ave E
Princeton, IL, 61356-2539

http://www.tetraresearch.com

Information

DUNS: 969308311

# of Employees: 2


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: Y



Award Charts




Award Listing

  1. Liquid Injection Modeling for High Enthalpy Air Breathing Propulsion Applications

    Amount: $149,992.00

    A critical aspect of high-speed air-breathing propulsion systems is liquid fuel injection into supersonic flow.The lack of understanding of primary and secondary breakup of liquid columns into droplet ...

    SBIRPhase I2019Department of Defense Air Force
  2. Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities

    Amount: $750,000.00

    Rigorous ground testing mitigates space propulsion system risk by enabling advanced component and system level rocket propulsion development and by demonstrating that designs reliably meet the specifi ...

    SBIRPhase II2017National Aeronautics and Space Administration
  3. Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities

    Amount: $125,000.00

    Rigorous ground testing mitigates space propulsion system risk by enabling advanced component and system level rocket propulsion development and by demonstrating that designs reliably meet the specifi ...

    SBIRPhase I2016National Aeronautics and Space Administration
  4. Efficient High Fidelity Computational Tool for Acoustically Driven Multiphysics Propulsion Modeling

    Amount: $125,000.00

    It is widely recognized that detailed simulation of large combustors to assess combustion instability and water spray systems to suppress rocket launch and test stand acoustic energy require advances ...

    STTRPhase I2016National Aeronautics and Space Administration
  5. Radiation Model Development for Combustion Systems

    Amount: $150,000.00

    Evolving demand for robust and accurate multi-physics modeling tools for high performance combustion devices is being driven by increasingly complex design, analysis, and simulation requirements, but ...

    SBIRPhase I2014Department of Defense Air Force
  6. Advanced Flow Analysis Tools for Transient Solid Rocket Motor Simulations

    Amount: $749,819.00

    The goals of reducing total cost and increasing reliability and safety of access to space continue to be top priorities for NASA. The most immediate propulsion launch challenge involves increasing li ...

    STTRPhase II2012National Aeronautics and Space Administration
  7. Advanced Flow Analysis Tools for Transient Solid Rocket Motor Simulations

    Amount: $100,000.00

    The challenges of designing, developing, and fielding man-rated propulsion systems continue to increase as NASA's mission moves forward with evolving solid propulsion requirements. Recent develo ...

    STTRPhase I2011National Aeronautics and Space Administration
  8. Multi-Phase Flow Analysis Tools for Solid Motor Applications

    Amount: $600,000.00

    The challenges of designing, developing, and fielding man-rated propulsion systems continue to increase as NASA's Vision for Space Exploration Program moves beyond the Space Shuttle and RSRM. The num ...

    STTRPhase II2009National Aeronautics and Space Administration
  9. Two Phase Flow Tools for Solid Motors with Dynamic Burning Surface Recession

    Amount: $100,000.00

    The challenges of designing, developing, and fielding advanced propulsion systems continue to increase as NASA's Vision for Space Exploration Program moves forward with new solid propulsion elements ( ...

    STTRPhase I2009National Aeronautics and Space Administration
  10. Multi-Phase Flow Analysis Tools for Solid Motor Applications

    Amount: $100,000.00

    The challenges of designing, developing, and fielding man-rated propulsion systems continue to increase as NASA's Vision for Space Exploration Program moves beyond the Space Shuttle and RSRM. The num ...

    STTRPhase I2008National Aeronautics and Space Administration
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