EMPIRICAL SYSTEMS AEROSPACE, INC.

Address

561 AIR PK DR HANGAR #D
OCEANO, CA, 93445-9665

http://www.esaero.com

Information

DUNS: 149341534
# of Employees: 20

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  1. Continued Development of Environmentally Conscious "ECO" Transport Aircraft Concepts as Hybrid Electric Distributed Propulsion Research Platforms

    Amount: $746,533.00

    ESAero's vast TeDP and HEDP-specific experience, Helden Aerospace's distributed propulsion airframe integration effects & CFD analysis experience, and Rolls-Royce's propulsion and power, thermal manag ...

    SBIRPhase II2016National Aeronautics and Space Administration
  2. Physics-Based Conceptual Design Flying Qualities Analysis using OpenVSP and VSPAero

    Amount: $121,408.00

    NASA?s OpenVSP tool suite provides a common parametrically driven geometry model formany different analyses for aircraft and is primarily used in the conceptual design phase. The current 3.5.1 release ...

    SBIRPhase I2016National Aeronautics and Space Administration
  3. OpenVSP Smart Conceptual Design Tool Improvements, Including Aerodynamic Analysis, Conformal Feature, and Structure Modeling

    Amount: $744,505.00

    ABSTRACT:The advancements to NASA's Vehicle Sketch Pad (OpenVSP 3.0) completed in 2014 evolved the software into a useful parametric graphics tool for serious aerospace design and analysis. ESAer ...

    SBIRPhase II2015Department of Defense Air Force
  4. Hybrid-Electric Rotorcraft Tool Development, Propulsion System Trade Space Exploration, and Demonstrator Conceptual Design

    Amount: $749,887.00

    Hybrid-electric propulsion is becoming widely accepted as a potential disruptive technology for aircraft that can provide significant reduction in fuel consumption as well as many other benefits. The ...

    SBIRPhase II2015National Aeronautics and Space Administration
  5. Cryogenic and Non-Cryogenic Hybrid Electric Distributed Propulsion with Integration of Airframe and Thermal Systems to Analyze Technology Influence

    Amount: $122,030.00

    A design iteration of ESAero's ECO-150 split wing turboelectric distributed propulsion (TeDP) concept is proposed to incorporate recent lessons learned in synergistic configuration opportunities, prop ...

    SBIRPhase I2015National Aeronautics and Space Administration
  6. OpenVSP Smart Conceptual Design Tool Improvements, Including Inboard Profile Visualization

    Amount: $149,994.00

    Recent advancements to NASA's Vehicle Sketch Pad (OpenVSP 3.0) have evolved the software into a useful parametric graphics tool for serious aerospace design and analysis. The proposed effort will ...

    SBIRPhase I2014Air Force Department of Defense
  7. Hybrid-Electric and All-Electric Rotorcraft Analysis and Tool Development

    Amount: $123,201.00

    During this Phase I effort ESAero will draw upon its knowledge of hybrid-electric propulsion system design and analysis for fixed wing aircraft to investigate the potential benefits of incorporating s ...

    SBIRPhase I2014National Aeronautics and Space Administration
  8. Physics-Based Radiator Design, Sizing & Weight Estimation Tool for Conceptual Design of More-, Hybrid-, and All-Electric Next Gen Aircraft

    Amount: $124,757.00

    Hybrid electric distributed propulsion (HEDP) systems have proven worthy for further consideration by approaching NASA's goals for N+2 and N+3 energy consumption, noise, emission and field length. The ...

    SBIRPhase I2014National Aeronautics and Space Administration
  9. ePHM System Development, Hardware-in-the-Loop Testing, Fault Tree, and FMECA Applied to and Integrated on NASA Hybrid Electric Testbeds

    Amount: $745,026.00

    Hybrid-Electric distributed propulsion (HEDP) is becoming widely accepted and new tools will be required for future development with validation and demonstrations during ground and eventually flight t ...

    SBIRPhase II2014National Aeronautics and Space Administration
  10. Physics-Based Wing Structure Design, Analysis and Weight Estimation Conceptual Design Tool for Hybrid Electric Distributed Propulsion

    Amount: $122,922.00

    As HEDP systems have proven worthy of further consideration by approaching NASA's goals for N+2 and N+3 energy consumption, noise, emission and field length, conceptual design tools to expedite the de ...

    SBIRPhase I2014National Aeronautics and Space Administration

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