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Company Information
SAN DIEGO, CA 92128-4424
United States



# of Employees: 187

Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No

Success Stories

  1. SBIR-STTR-Tibbetts Award Winner - ATA Engineering, Inc.

    2020 Tibbetts Award Winner ATA has created & validated a suite of modeling & simulation tools to aid in the development & fielding of highly-engineered systems.                    ...

Award Charts

Award Listing

  1. Optimization of Fatigue Test Signal Compression Using the Wavelet Transform

    Amount: $124,883.00

    Traditional approaches to accelerated fatigue testing rely on heuristic methods with thresholds based mostly on experience and engineering judgment. These methods generally do not apply to the multiax ...

    STTRPhase I2018Department of Defense Navy
  2. Short Fiber Composite Mechanical Property Modeling and Prediction Framework

    Amount: $149,858.00

    Compression-molded short-fiber composite (SFC) materials have several advantages over metallic and continuous-fiber composite (CFC) materials, including greater part complexity, improved dimensional s ...

    SBIRPhase I2018Department of Defense Air Force
  3. 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
  4. 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
  5. 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
  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. 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
  8. 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
  9. Analysis Tools for Composite Laminate Material Properties Prediction

    Amount: $999,248.10

    ATA Engineering proposes to enhance and validate an innovative software toolset, known as COMPAS, for predicting the performance of fiber-reinforced polymer matrix composite laminate materials. The so ...

    SBIRPhase II2017Department of Defense Army
  10. Fully Integrated Aeroelastic Simulation of Complete Vertical Lift Configurations

    Amount: $996,183.20

    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 II2017Department of Defense Army
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