EMPIRICAL SYSTEMS AEROSPACE INC
Megawatt-class traction inverter for aircraft propulsion with 2-3x weight reduction and 99.5% efficiency
- Sector
- Aerospace
- Headquarters
- San Luis Obispo, CA
- Total capital
- $51.2M
- Federal grants
- $10M
- 20 awards · 2015–2024
- Rank in peer group#27 of 155
- Private capital raised
- None on recordNo Form D filings on SEC EDGAR. Some raises are not filed.
- Federal contracts
- $41.2M
- 58 awards · NASA, Defense
- Rank in Aerospace#90 of 1335
- Granted patents
- None on recordNo USPTO grants. Applications publish after 18 months.
Capital timeline
Latest events
- Federal grantDefense · Phase II · Project Capture: Capturing Aerial Payloads To Unleash Reliable Exploitation$1.0M
- Federal contractDefense · Project Capture: Capturing Aerial Payloads To Unleash Reliable Exploitation$1.0M
- Federal contractDefense · Hydrogen Propulsion Energy Module For Aircraft Sizing And Analysis$75K
- Federal grantDefense · Phase I · Hydrogen Propulsion Energy Module For Aircraft Sizing And Analysis$75K
- Federal grantNASA · Phase I · Aircraft Traction Inverter for Hybrid-Electric and All-Electric Megawatt-Class Vehicles$150K
- Federal contractDefense · Electric Small Aircraft Air Launch Effect Via Valkyrie$74K
- Federal grantDefense · Phase I · ESAero NSN 6625-01-123-8721$44K
Show 71 earlier federal awards
- Federal grantNASA · Phase I · Wind Tunnel and Flight Testing of Scalable Modular Aerial Research Testbed$149K
- Federal grantDefense · Phase I · Gaseous Hydrogen Smart Storage System$140K
- Federal contractDefense · Es Aero Ale Cta$1.0M
- Federal grantDefense · Phase I · Attritable Swarming Long-endurance Drone (ASLED)$120K
- Federal grantDefense · Phase II · Electrified Rotor Head for Advanced Vertical Flight$750K
- Federal grantDefense · Phase I · Application Study for Contrarotating Electric propulsioN sysTem foR hIgh effiCiency (CENTRIC)$50K
- Federal contractNASA · Onboard Prognostics And Health Management For Uam Using Machine Learning Techniques$124K
- Federal grantDefense · Phase I · AF211-CS01 Phase I$50K
- Federal contractNASA · Technical Challenge Assessment Support For The X-57 Project$165K
- Federal contractDefense · SBIR R&d$487K
- Federal contractDefense · To Develop An Electrified Smart Rotor Head To Enable Unique Aircraft Configurations By Significantly Reducing The Mechanical Complexity Of Existing Variable Blade Pitch Rotor Heads Seen On Traditional Aircraft Such As Helicopters And TILT‐ROTORS$147K
- Federal contractNASA · The Purpose Of This Task Order Is To Provide The Testing Of An X-57 Cruise Propulsion Module In Accordance With The Performance Work Statement Entitled "cruise Motor&cruise Motor Controller Performance Testing" Dated: May 8, 2020.$154K
- Federal grantDefense · Phase I · Agile manufacture and distribution of the Field Adaptable Supply Technology (FAST) swarming system$198K
- Federal grantDefense · Phase II · Propulsion integration for low-cost, extended-range, attritable UAS$1.5M
- Federal contractNASA · X-57 Mod IV Support Through Acceptance Of High Lift Flight Hardware.$3.9M
- Federal contractNASA · The Purpose Of This Task Order Is To Provide Software Development, Testing And Support For The X-57 Project.$809K
- Federal contractNASA · Battery Control Module Upgrade Support$470K
- Federal contractNASA · Troubleshoot Of Hmlc Developmental Software$23K
- Federal contractNASA · Esaero Mod II Support Task Order For The Continued Development, Integration, And Testing Activities Required To Meet Afrc#s Airworthiness Requirements$3.5M
- Federal contractNASA · This Task Order Is Issued To Expand Scope Of Testing Of Cruise Motors And Cruise Motor Controllers (cmcs)for The X-57 Aircraft.$417K
- Federal contractNASA · Validation Of Uam Dynamics Modeling Tool Suite Using Scaled Modular Aerial Research Testbed.$748K
- Federal contractNASA · This Task Order Is Issued In Support Of Mod III Wing&system Integration. Work Shall Be Accomplished In Accordance With Attached Performance Work Statement Entitled: "mod III Wing&system Integration Follow-on" Dated 30 May 2019.$3.8M
- Federal grantDefense · Phase II · Smart Aircraft Conceptual Design in Multidisplinary Design Optimization$3M
- Federal contractNASA · The Aquifer Program Looks To Tackle Two Major Forward Looking Issues With The Cas Project. Safety Issues With The Use Of Battery Technology For Electric Aircraft Noise Reduction Of Commercial Aviation Aircraft For The Pursuit Of An All/partial Electric Aircraft, Integration Of The Batteries To Prevent Cell To Cell Propagation And Thermal Runaway Present A Significant Safety Concern That Must Be Address For Any Design. Additionally, Batteries Also Present Issues In Terms Of Charging Logistics$300K
- Federal contractNASA · Complete Integration And Test For The Sceptor Mod II Configuration$1.4M
- Federal contractNASA · NASA Aircraft X-57 Mod IV Support Through Critical Design Review.$1.7M
- Federal grantNASA · Phase II · Demonstration of Autonomous Differential Throttle-based Flight Control for Aircraft with Distributed Electric Propulsion$749K
- Federal contractNASA · Task Order For Software Test Support For Sceptor Flight Critical Software$66K
- Federal contractNASA · Igf::ot::igf This Task Order Is Issued To Perform In Cooperation With NASA The Integration Of The Electric Propulsion System For The X-57 Aircraft. The Contractor Shall Provide Continued Engineering Services To Integrate The Electrical Motors Into The Tecnam Engine Nacelles, And Perform The Required Traction System, Command System, And Instrumentation Integration In The Aircraft.$399K
- Federal grantNASA · Phase I · Integrated Autonomous Controller with Health State Awareness.$125K
- Federal grantNASA · Phase I · UAM Disturbance Rejection in Conceptual Design$125K
- Federal grantNASA · Phase I · Sampling the Venusian Atmosphere Using a Solar Power Paraglider$125K
- Federal contractNASA · Structural Fabrication Of A New Wing To Replace The Existing Wing On The Tecnam P2006T Aircraft And The Fuselage Interface Assemblies Required To Interface The Wing To The Fuselage. Key Tasks To Be Performed Under This Task Order Include The Following: The Contractor Will Populate The Completed Mod III Wing With Flight Systems To The Maximum Extent Possible, The Contractor Will Structurally Integrate The Mod III Wing To The Fit Check Fuselage At The Contractors Facility.$766K
- Federal contractNASA · Igf::ot::igf Mod Ii_iv Fuselage To Wing Fairing Engineering Services$380K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$120K
- Federal contractNASA · Igf::ot::igf$653K
- Federal contractNASA · Igf::ot::igfopen Vehicle Sketch Pad Is An Open-source Parametric Aircraft Geometry Tool That Allows Users To Create A 3D Surface Model Defined By Common Engineering Parameters. Openvsp Has Thrived As Mainline Geometry Tool For Aerospace Applications Through Its Ease Of Use, Flexibility, Scripting, Broad Range Of Geometry Outputs, And Community Support. Continued Development Further Enhances The Software Capabilities While Improving Robustness.$50K
- Federal contractNASA · Igf::ot::igfigf::ot::igf Design And Integration Of A Secondary Egress Option For X-57$144K
- Federal contractNASA · Igf::ot::igf The Contractor Will Perform In Cooperation With NASA The Design And Integration Of An Electric Propulsion System For The Scalable Convergent Electric Propulsion Technology Operational Researcher (sceptor) Project. The Sceptor Project Will Retrofit A Production Tecnam P2006T Aircraft (minus The Rotax Engines) With An Electric Propulsion System. Two Aircraft Subsystems, The Cruise Motor Controller (cmc) And The Battery Management System (bms), Contain Safety Critical Software. In O$250K
- Federal contractNASA · Igf::ot::igfigf::ot::igf Procurement Of Additional X-57 Cruise Motors And Controllers$260K
- Federal grantNASA · Phase I · Onboard Generic Fault Detection Algorithm Development and Demonstration for VTOL sUAS$125K
- Federal contractNASA · Igf::ot::igf In The Proposed STTR Study, Empirical Systems Aerospace, Inc. (esaero) And The University Of Illinois At Urbana-champaign (uiuc) Will Create A Methodology For The Development Of A Flight Control Algorithm Featuring Differential Thrust Provided By A Distributed Electric Propulsion (dep) System. The Focal Piece Of The Study Is A Dynamically Scaled Cirrus SR22T UAV At Uiuc, Which Will Be Modified To Include Multiple Electrical Ducted Fans (edf) Arranged To Exhibit Strong Propulsion-ai$125K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$226K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$666K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$100K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$65K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$44K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$16K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$661K
- Federal contractNASA · Igf::ot::igf Empirical Systems Aerospace Will Design And Plan A Test And Evaluation Program To Develop Requirements, Techniques, Tools And Procedures For Testing Tightly Integrated Pai Systems. A Systems Employing A Wingtip Mounted Propeller And/or Turbine Will Be Tested Because It Is Illustrative Of The Inherent Challenges Of Testing Pai Systems In Flight. This Project Will Not Develop A Complete Aircraft; Instead It Will Develop A Test Apparatus That Can Be Mounted On Another Aircraft Or Wi$814K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$1.8M
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$2.6M
- Federal contractNASA · Igf::ot::igf Nasas 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 Currently Contains Significant Gaps When Assessing Handling Qualities For A Particular Configuration Forcing The Engineer To Rely On Historical Methods With Limited Applicability To Advanced Technology Design Concepts With Unconventional Configurations. In The Proposed Effort, Esaero W$121K
- Federal contractNASA · Igf::ot::igf Structural Design Of A Wing And Fuselage Interface Assemblies For The Scalable Convergent Electric Propulsion Technology Operational Researcher (sceptor) Project.$605K
- Federal contractNASA · Igf::ot::igf Scalable Convergent Electric Propulsion Technology For Operations Research (sceptor) Software$351K
- Federal grantNASA · Phase II · Continued Development of Environmentally Conscious "ECO" Transport Aircraft Concepts as Hybrid Electric Distributed Propulsion Research Platforms$747K
- Federal contractDefense · Igf::ot::igf SBIR Phase II - Openvsp Smart Conceptual Design Tool$644K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$300K
- Federal contractNASA · Igf::ot::igf In Order To Design, Analyze, Build, Test Operate, Maintain And Sustain The Cept For The Research Phase, NASA Afrc Requires The Engineering And Technical Support Of Esaero Which, As The Dep Wing Prime Contractor, Has The Unique Knowledge And Possesses Proprietary Information Of The Dep Wing And Associated Sub-systems. This Effort Includes The Modification Of An Existing Ga Aircraft With NASA Furnished Electric Motors, NASA Driven Power Management And Distribution System Design, Into$5.1M
- Federal contractNASA · Igf::ot::igf 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, Propulsion And Thermal Management System Research And Tool Development, And Aeropropulsive Benefits Reported By Lockheed Martin. Non-cryogenic And Cryogenic/superconducting Components Will Be Included In Three Separate Propulsion System Architectures: One Cooled Via Conventional "warm" Cool$122K
- Federal grantNASA · Phase II · Hybrid-Electric Rotorcraft Tool Development, Propulsion System Trade Space Exploration, and Demonstrator Conceptual Design$750K
- Federal contractNASA · Igf::ot::igf 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 Design Cycle Are Desired. During This Phase I Effort Esaero Will Progress The Development Of The Hybrid-electric Distributed Propulsion (hedp) Togw Tool Developed In The Previous Phase I SBIR (NNX13CC24P) By Producing A Physics-based Wing Structure Analysis And Weight Estimation Module. T$123K
- Federal contractNASA · Igf::ot::igf 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 Thermal Management Associated With These Systems Has Been Recognized As A Major Challenge To Be Overcome. Esaero's Recent 2012 Phase I SBIR (NNX13CC24P) Identified The Radiator As A Driving Component Within The Thermal Management System (tms). Its Design Has Profound First Order Effec$125K
- Federal contractNASA · Igf::ot::igf 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 Such Systems Into Rotorcraft Designs. Past Rotorcraft Studies Have Been Conducted In Conjunction With Electricore, Inc. And An Industry Prime, To Develop Hybrid Propulsion System Trade Studies And Develop Databases For Hybrid Propulsion System Worthy Components. This Knowledge Will Be L$123K
- Federal contractDefense · Igf::ot::igf SBIR 1 - Openvsp Smart Conceptual Design Tool Improvements$150K
- Federal contractNASA · Igf::ot::igf 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 Testing. Intelligent Health Management Will Be Paramount To Any Future Ground And Flight Testing Activities Planned By The Industry On Hedp Systems. To Support This, An Intelligent Prognostics And Health Management (ephm) System Will Be Designed And Executed For The Hedp System On The N$1.1M
- Federal contractNASA · Design And Fabricate A Hybrid Electric Integrated System Testbed (heist) The Goal Of The SBIR Phase III Work Is To Design And Assemble A Static Distributed Propulsion Test Stand To Complete Ground Testing And Early Controller And Power Management Research Scaled To Model A Generic Small Airborne Test-bed.$1.3M
- Federal contractNASA · Igf::ot::igf Hybrid-electric Distributed Propulsion (hedp) Is Becoming Widely Accepted And New Tools Will Be Required For Future Development. This Phase I SBIR Proposal Creates A Turbo-electric, Hybrid Electric Propulsion System Sizing And Weight Synthesis Tool Specifically Designed For Use In An Mdao Framework. It Will Offer Significant Flexibility Regarding Placement Of The Propulsive Devices For Top-level Hybrid Design, Including Over-wing, Under-wing, Splitwing, Fuselage Pylon-mounted, And $121K
- Federal contractNASA · Igf::ot::igf 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 Testing. To Monitor The Overall Hedp System Health In Real Time, A Virtual Requirement To Flight Qualify Any Architecture Hardware Components, Reliability Centered Maintenance (rcm) Applied To Prognostics And Health Management (phm) Will Yield Significant Improvement In Hedp System Relia$124K
- Federal contractNASA · A Baseline Propulsion System Has Been Designed As A Starting Point In A Previous SBIR Effort For This Project Which Consists Of Two Turboshaft Engines, A Generator Coupled Directly (no Gearbox) With Each Engine, And Electric Cables To Motors That Drive Shrouded Fans Installed In Or Over The Wing. For This Baseline, There Are Eight Fans Per Wing, And The Turboshaft Engines Use Kerosene Fuel As The Energy Source. One Major Issue Faced By This Type Of Configuration Is The Propulsion Integration Of $100K
- Federal contractNASA · Integration Of An Advanced Cryogenic Electric Propulsion System (aceps) To Aerodynamically Efficient Subsonic Transport Aircraft This Proposal Defines Innovative Aerodynamic Concepts And Technology Goals Aimed At Vehicle Efficiency For Future Subsonic Aircraft In The 2020 2030 Timeframe. Noise, Emissions And Fuel Burn Are All Vehicle Efficiency Concerns Which Can Be Addressed By Aerodynamic Concepts Either On The Component, Subsystem, Or Aircraft Design System Level. In Line With The NASA, An As$100K
Federal awards are summed by year (78 awards); hover a bar for the split. Form D reports securities sold, which can differ from an announced round; filings are numbered in the order they were made.
Standing among 155 peers
Line = medianAerospace · Components · Device
- Federal grants#27 · top 17%
Cumulative measures favor older companies. Rankings describe position today, not outcome. Below the median, ranks show as a band rather than a number.
Founders and team
No founders are linked to this company yet.
Founders appear once a person is matched to the company through its own patents, grants or filings. We never infer people from social profiles.
Checked: USPTO inventors; federal award principal investigators; SEC Form D related persons · Oct 23, 2026
Claim this profile to add your teamWhat it has protected
No granted patents are on record.
USPTO usually publishes applications 18 months after filing, so recent applications may not be visible yet. Patents assigned under a different entity name won’t match.
Checked: USPTO granted patents and published applications · Oct 23, 2026
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Regulatory activity · Aerospace
- Nondiscrimination in Federally Assisted Programs of NASA-Effectuation of Title VI of the Civil Rights Act of 1964National Aeronautics and Space Administration
- Special Conditions: AMAC Aerospace, The Boeing Company Model 747- 8 Airplane; Side-Facing SeatsFederal Aviation Administration
- Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous AmendmentsFederal Aviation Administration
- Operating Limitations at John F. Kennedy International AirportFederal Aviation Administration
- Operating Limitations at New York LaGuardia AirportFederal Aviation Administration
- Special Conditions: Honeywell Aerospace US LLC, Dassault Aviation Model Falcon 900EX Airplane; Electronic System Security Protection From Unauthorized External AccessFederal Aviation Administration
Rules are matched to sector, not to company. Recent activity in a sector is context rather than a signal about this business — until rules are matched to what a company actually builds, the section is shown as context and nothing more.
Sources
Federal grants from SBIR/STTR, NIH, NSF and DoD records. Federal contracts from USAspending.gov. Private capital from SEC Form D. Patents from USPTO. Publications from OpenAlex. Regulatory activity from the Federal Register. Press matched on company name.
How to read this page
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Data freshness
SEC Form D filings through . SBIR and STTR awards through .