ATA Engineering, Inc.

Company Information
Address 13290 Evening Creek Dr S Ste 250
San Diego, CA, 92128-4695

http://www.ata-e.com

Information

DUNS: 133709001

# of Employees: 151


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Continuous-Scan Phased Array Measurement Methods for Turbofan Engine Acoustic Testing

    Amount: $749,885.00

    To allow aviation growth to continue in the face of increasingly stringent noise pollution standards, new aircraft engines must be designed with noise performance as a principal constraint. Technologi ...

    SBIRPhase II2017National Aeronautics and Space Administration
  2. Multiphysics Framework for Prediction of Dynamic Instability in Liquid Rocket Engines

    Amount: $124,819.00

    Mitigation of dynamic combustion instability is one of the most difficult engineering challenges facing NASA and industry in the development of new continuous-flow combustion systems such as the combu ...

    STTRPhase I2017National Aeronautics and Space Administration
  3. Design Tool and Methodology for Verification of Submarine Finite Element Models

    Amount: $129,687.00

    Shipyards are responsible for creating and analyzing finite element (FE) models of submarine pressure hulls and components under hydrostatic pressure loading, whereas the Navy technical community is r ...

    SBIRPhase I2017Department of Defense Navy
  4. Flexible Software Toolset for Accurate Prediction of High-Speed Wind Tunnel Transient Airloads

    Amount: $149,944.00

    High-speed wind tunnel test articles and support systems experience violent unsteady airloads associated with tunnel startup/shutdown and model insertion in tunnels with injection capabilities. Curre ...

    SBIRPhase I2017Department of Defense Air Force
  5. Prediction of Rotor Loads from Fuselage Sensors for Improved Structural Modeling and Fatigue Life Calculation

    Amount: $129,893.00

    ATA Engineering and researchers at the Georgia Institute of Technology will develop a framework for the accurate reconstruction of rotor loads from a suite of fixed-frame fuselage sensors that are uti ...

    STTRPhase I2017Department of Defense Navy
  6. A Multiphysics Framework Utilizing Nonlinear Material Models for Predicting Impact of Structural Profile Disruption on High-Velocity Air Vehicles

    Amount: $149,742.00

    The aerothermal environment for hypersonic flight vehicles is severe and can generate extremely high material temperatures. These high-temperature environments can cause intense localized heating, whi ...

    STTRPhase I2017Department of Defense Air Force
  7. Continuous-Scan Phased Array Measurement Methods for Turbofan Engine Acoustic Testing

    Amount: $124,832.00

    ATA Engineering, Inc., (ATA) proposes an SBIR project to advance the technology readiness level (TRL) of a method for measuring phased array acoustic data for complex distributed noise sources using c ...

    SBIRPhase I2016National Aeronautics and Space Administration
  8. Improved Efficiency of Small Core Turbines through Tip Leakage and Secondary Flow Mitigation

    Amount: $124,751.00

    NASA's Aeronautics Research Mission Directorate has declared ultra-efficient commercial air vehicles a strategic area for development in the coming decade. With no foreseeable alternatives, advanced g ...

    SBIRPhase I2016National Aeronautics and Space Administration
  9. Advanced Reentry Aeroheating Simulation Framework

    Amount: $124,955.00

    Vehicle reentry presents numerous challenges that must be carefully addressed to ensure the success of current and future space exploration missions. As they enter the atmosphere, these vehicles are s ...

    SBIRPhase I2016National Aeronautics and Space Administration
  10. Fully Integrated Aeroelastic Simulation of Complete Vertical Lift Configurations

    Amount: $99,973.97

    Current approaches for resolving rotorcraft fuselage responses in the presence of aerodynamic/structural excitation require ample conservatism because current CFD-based aeromechanic solutions lack the ...

    SBIRPhase I2016Department of Defense Army

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