Experimental Aircraft: Comparative Analysis of Governance, Funding, and Business Models
Abstract
1. Introduction
2. Methodology
2.1. Analytical Framework
- What governance, funding, and business models are employed in existing experimental aircraft programs worldwide?
- How do these models relate to platform scale, sectoral orientation (civil, defence, or dual-use), and strategic objectives?
- What lessons can be derived from existing experimental aircraft programs to inform the development of a future European experimental aircraft?
2.2. Data Structure and Compilation of EA Data
3. Results and Analysis
3.1. Governance Models
3.2. Funding Models
3.3. Business Models
3.4. Interconnections Between Funding, Business, and Governance Models
3.4.1. Interplay Between Funding and Business Models of EA
Public and Public–Private Funding
Private Funding
Academic and Government Grants
3.4.2. Interplay Between Governance Structures and Funding Models
Government-Led or Public Institution Governance
Corporate Governance
University Governance
3.5. Contextual Aspects of EA
3.5.1. Scale and Type of EA
Scale in Relation to Funding and Governance Models
- Full-Scale Experimental Aircraft
- Sub-Scale Experimental Aircraft
3.5.2. Regional Aspects
Geographic Distribution of EA
- Europe and the USA frequently utilize public–private partnerships backed by strong institutional support from, for example, the EU Horizon programs, NASA, and the U.S. Department of Defense (DoD).
- Japan and India predominantly rely on government and defence ministry funding, with projects often fully publicly funded and oriented towards technology demonstration.
- Emerging markets like Turkey and Israel exhibit mixed funding models, combining private investment with indirect public support for strategically important projects.
3.5.3. Civil, Defence, and Dual-Use Applications
3.5.4. Launch and Operational Period Trends
- Early testbeds and demonstrators (1980s to 2000s) primarily concentrated on crewed, full-scale aircraft, with substantial government defence involvement. These platforms were designed for traditional aerospace applications, emphasizing established propulsion and avionics technologies.
- More recent projects (2010s onward) show a marked shift toward electric and hydrogen propulsion, urban air mobility (UAM), and uncrewed aerial vehicles (UAVs). This transition mirrors broader trends toward sustainability, autonomy, and innovative air transport concepts.
- There is an emerging trend of commercialization of full-scale EA, signalling a movement away from purely research.
3.5.5. Organizational Involvement Patterns
- Large aerospace corporations such as Airbus, Boeing, and Rolls-Royce dominate full-scale projects, frequently collaborating with government aviation and defence agencies to leverage resources and strategic capabilities.
- Universities and research centres—including institutions like NLR, TU Delft, NASA research centres, and various international universities—primarily lead or contribute to sub-scale and uncrewed platforms, focusing on innovation, fundamental research, and technology validation.
- Complex full-scale projects often involve multi-organization consortia that span national boundaries and sectoral domains, combining expertise from industry, academia, and government to address the multifaceted challenges of modern aerospace development.
4. Discussion—Lessons Learned from EA
4.1. Key Lessons on Flight Testing, Collaboration, and Technology Challenges
4.2. Collaborative Governance Is Key to Flying Research Platforms Success
4.3. Funding Patterns Reflect the Strategic Nature of Experimental Aircraft
4.4. Scale and Sectoral Leadership Vary with Governance and Funding
4.5. Public–Private Partnerships Enable Risk Sharing and Innovation
4.6. Geographic and Regional Nuances Shape Flying Research Platforms Ecosystems
4.7. Experimental Aircraft Are Primarily Strategic Innovation Platforms
4.8. Flight Testing and Certification Require Early and Sustained Investment
4.9. Modularity and Flexibility Enhance Testbed Value and Longevity
4.10. Technology-Specific Funding and Governance Adaptations Are Necessary
4.11. Cross-Disciplinary Collaboration and Multi-Stakeholder Networks Are Essential
5. Conclusions
Author Contributions
Funding

Data Availability Statement
Conflicts of Interest
Appendix A. Complete Excel Table, Including Dataset and Literature Sources
| Testbed Name | ID No | Country | Governance Model | Business Model | Key Technologies | Scale | Launch Year | End of Operations | Crewed/Uncrewed | Civil/Defence–Military/Dual | Source |
| Boeing ecoDemonstrator | EA_0001 | USA | C.G | T&I | SAFs, Flight Controls, Operational and Load Optimization, Environmental Impact | full | 2012 | ongoing | Crewed | Civil | [15,51,52,53,54,55,56,57,58] |
| Airbus Flightlab—BLADE EA demonstrator | EA_0002 | France | P.P. | T&I | Aerodynamic Design, Emissions, Data Connectivity | full | 2010 | ongoing | Crewed | Civil | [6,59,60,61,62,63,64,65,66] |
| Airbus UPNEXT | EA_0003 | France | C.G | T&I | Aerodynamic Design, New Fuels | full | 2020 | ongoing | Crewed | Civil | [16,67,68,69,70,71,72,73,74] |
| Airbus A310 MRTT | EA_0004 | Spain | C.G | T&I | Air Refueling, Systems Integration and Testing | full | 2006 | 2023 | Crewed | Civil | [75,76,77,78,79,80,81,82] |
| Airbus A350 XWB Testbed | EA_0005 | France | C.G | T&I | Aerodynamical and Structural Design, Engine Testing | full | 2012–2013 | ongoing | Crewed | Civil | [37,83,84,85,86,87,88,89] |
| Rolls-Royce’s “Spirit of Innovation” | EA_0006 | UK | P.P | T&I | Energy Systems, Structural Design and Thermal Testing | full | 2019 | 2022 | Crewed | Civil | [22,90,91,92,93,94,95,96,97,98,99,100] |
| NASA X-57 Maxwell | EA_0007 | USA | P.G. | T&I | Flight Systems, Avionics | full | 2016 | 2023 | Crewed | [10,18,101,102,103,104,105,106,107,108,109,110] | |
| ZeroAvia’s Hydrogen-Powered Aircraft | EA_0008 | UK | P.P. | T&I | Hydrogen Fuel Cells, Power Electronics | sub | 2019–2020 | ongoing | Crewed | [34,111,112,113,114,115,116,117,118,119,120,121,122,123] | |
| Joby Aviation|Joby | EA_0009 | USA | C.G. (before 2021) P.P. (after 2021) | C.F | eVTOL, Electric Propulsion, Noise Reduction | full | 2015 | ongoing (planned to be commercialized) | Crewed | [36,124,125,126,127,128,129,130,131,132,133,134] | |
| Lilium Jet | EA_0010 | Germany | C.G. | C.F | Electric Ducted Fans, Li-ion Batteries, Fly-by-Wire | full | 2017 | 2024 | Crewed | [135,136,137,138,139,140,141,142,143,144,145,146] | |
| Alice Aircraft by Eviation Aircraft | EA_0011 | Israel | C.G | C.F | Electric Propulsion, Battery System, Composite Airframe | full | 2019 | 2025 (paused) | Crewed | [28,147,148,149,150,151,152,153,154,155] | |
| Urban Aeronautics’ CityHawk | EA_0012 | Israel | C.G | C.F | Ducted-Fan VTOL, Hydrogen Fuel Cells | full | 2017 | ongoing (to be commercialized) | Crewed | ||
| Vertical Aerospace (eVTOL Aircraft) | EA_0013 | UK | C.G | C.F | DEP, Lightweight Composites, Low-Noise Design | full | 2018 (first flight) | ongoing (to be commercialized) | Crewed | [156,157,158,159,160,161,162,163] | |
| General Electric Boeing 747-400 jumbo jet | EA_0014 | USA | C.G | T&I | Turbofan Engines, FADEC, Aero Testing | full | 2010 | 2018 | Crewed | [164,165,166,167] | |
| Rolls Royce Boeing 747-200B | EA_0015 | UK | C.G | T&I | Engine Integration, Instrumentation | full | early 1980s | late 2000s | Crewed | [167,168,169] | |
| Airbus EcoPulse (ΤΒΜ-900) | EA_0016 | France | C.G | T&I | HMI, AI-Assisted Operations | full | 2022 | ongoing | Crewed | [170,171,172,173,174,175,176,177,178,179] | |
| NLR Research Aircraft Cessna Citation II | EA_0017 | Netherlands | P.G. | T&I | Sensor Integration, Instrumentation | full | 1993 | ongoing | Crewed | [19,180,181,182] | |
| NLR SFD | EA_0018 | Netherlands | P.G. | T&I | DEP, Hybrid Propulsion, Advanced Controls | sub | 2017 | ongoing | Uncrewed | [13,183,184,185,186,187,188,189] | |
| NASA Gulfstream III Aerodynamics Research | EA_0019 | USA | P.G. | T&I | Morphing Wings, Aeroelastic Actuation | full | 2012 (first flight) | 2015 | Crewed | [47,190,191,192,193,194,195,196] | |
| NASA Langley ‘s AIRSTAR | EA_0020 | USA | P.G. | T&I | Subscale Testing, Adaptive Control, Telemetry | sub | early 2000s | ongoing (probably) | Uncrewed | [48,197,198,199,200,201,202,203] | |
| NASA F-15B TN 836 Aeronautics Research | EA_0021 | USA | P.G. | T&I | High-AOA Aerodynamics, Fly-by-Wire | full | late 1980s | late 2010s | Crewed | Defence–Military | [191,204,205,206,207] |
| E-FAN | EA_0022 | France | C.G | T&I | Electric Propulsion, Lightweight Composites | full | 2011 | 2017 | Crewed | Civil | [208,209,210,211,212] |
| E-FAN X | EA_0023 | UK | Collaborative Consortium Governance | T&I | Hybrid-Electric, High-Voltage Systems | full | 2017 | 2020 | Crewed | Civil | [24,213,214,215,216] |
| Boeing X-48 (2 models: X-48B and X-48C) | EA_0024 | USA | P.P. | T&I | BWB Aerodynamics | sub | 2005 | 2012–2013 | Uncrewed | Defence–Military | [21,217,218,219,220] |
| JetZero’s project | EA_0025 | USA | C.G | C.F | Aero Efficiency, Alternative Propulsion | sub | 2021 | ongoing | Uncrewed | Dual Use | [17,221,222,223,224] |
| Ilyushin Il-76 (many variants were developed) | EA_0026 | Russia | C.G P.G. | C.F | Heavy Transport, Turbofans, Rugged Airframe | full | 1971 | ongoing | Crewed | Defence–Military | [225,226,227,228,229,230] |
| Lockheed Martin CATBird (Cooperative Avionics Test Bed) | EA_0027 | USA | P.P. | T&I | Avionics, Autonomous Systems | full | 2007 | 2014 | Crewed | Defence–Military | [38,231,232,233,234,235] |
| MIT Lincoln Laboratory’s Airborne Sensor Test Bed | EA_0028 | USA | P.G. | T&I | EO/IR Sensors, Communications | full | 1990s | Ongoing | Crewed | Defence–Military | [236,237,238,239] |
| Lockheed Martin X-56 | EA_0029 | USA | P.P. | T&I | Uncrewed Systems, Advanced Controls | sub | 2013 (first flight) | 2017 | Uncrewed | Defence–Military | [240,241,242,243,244,245,246,247,248] |
| Boeing Phantom Ray | EA_0030 | USA | C.G | T&I | Stealth UAV, Autonomous Missions | full | 2010 | 2013 | Uncrewed | Defence–Military | [39,249,250,251,252,253,254,255] |
| Scaled Composites Proteus | EA_0031 | USA | C.G | C.F | High-Altitude Aerodynamics, Lightweight Composites | full | 1998 | ongoing | Crewed | Dual Use | [256,257,258,259,260] |
| Honeywell 757 Flying Testbed | EA_0032 | USA | C.G | T&I | Propulsion Testing, Avionics Systems | full | 2005 | ongoing | Crewed | Dual Use | [261,262,263,264,265,266,267] |
| Kawasaki XC-2 | EA_0033 | Japan | P.P | T&I | Composites, Turbofans, Fly-by-Wire | full | 2010 | ongoing | Crewed | Defence–Military | [23,268,269,270] |
| SWiFT (Stealth Wing Flying Testbed) | EA_0034 | India | P.G. | T&I | Stealth Wing, Autonomous Control | sub | 2022 | ongoing | Uncrewed | Defence–Military | [20,271,272,273,274,275] |
| Turkish Aerospace Industries (TAI) Anka UAV (1–3 variants) | EA_0035 | Turkey | C.G | T&I | UAV Autonomy, Stealth Design | full | 2022 | ongoing | Uncrewed | Defence–Military | [276,277,278,279] |
| Israel Aerospace Industries (IAI) Heron UAV | EA_0036 | Israel | P.P | C.F | EO/IR Sensors, SATCOM, Autonomous Ops | full | 1994 (first flight) | ongoing | Uncrewed | Defence–Military | [280,281,282,283,284,285,286,287] |
| DA 62—Diamond Aircraft | EA_0037 | Austria | C.G | C.F | Efficient Engines, Composite Airframe | full | 2012 | ongoing | Crewed | Civil use (private, training, utility aviation) | [30,288,289,290,291,292,293,294] |
| Zero-e | EA_0038 | France | P.P. | T&I | Hydrogen Combustion, LH2 Storage, Fuel Cells | full | 2020 | ongoing | Crewed | Civil Use | [43,295,296,297,298,299] |
| H2FLY HY4 | EA_0039 | Germany | C.C. | T&I | DEP, Aeroelastic Structures, Digital Twin | sub (1:5–1:3 scale of a regional airliner) | 2018 | 2023 | Uncrewed | Civil Use | [25,300,301,302,303,304,305,306,307,308] |
| Numerical Design Results Demonstrator (NORD) | EA_0040 | Poland | A.G. | T&I | Dynamic Stability, Flight Data Analysis | subd | early 2020s | possibly ongoing | Uncrewed | Civil | [309,310] |
| AlbatrossONE | EA_0041 | UK | C.G: | T&I | Hinged Wing-Tips, Gust Alleviation | subd | 2019 | ongoing | Uncrewed | Civil use | [311,312] |
| FLEXOP demonstrator | EA_0042 | Hungary | C.C. | T&I | Aeroelastic Tailoring, Flutter Control | full | 2015 | 2020 | Uncrewed | Civil use (potentially dual use) | [313,314,315,316] |
| e-Genius-Mod | EA_0043 | Germany | A.G. | T&I | Electric Motor, Battery System | full | 2022 | ongoing | Crewed | Civil Use | [27,317] |
| Scout B1-100 | EA_0044 | Switzerland | C.G | C.F | Autonomous Control, Robust Airframe | sub | mid-to-late 2010s or early 2020s | ongoing | Uncrewed | Civil | [44,318,319] |
| Cirrus SR22T | EA_0045 | USA | A.G. | R&E | DEP Propulsion | sub | 2017 | ongoing | Uncrewed | Civil | [40,320] |
| MAGMA | EA_0046 | UK | P.P. | T&I | Fluidic Controls, Circulation Control | sub | 2017 | early 2020s | Uncrewed | Civil | [35,321,322,323] |
| Super Guppy Foamie | EA_0047 | USA | P.G. | T&I | Scaled Model, Balloon Launch | sub | around 2012 | ongoing | Crewed | Civil | [49,324,325] |
| GA-USTAR aircraft | EA_0048 | USA | A.G. | R&E | Dynamic Scaling, Flight Data Systems | sub | 2017 | ongoing | Uncrewed | Civil | [32,326,327] |
| UIUC Subscale Sukhoi | EA_0049 | USA | A.G. | R&E | Scaled Aerodynamics, High-Precision Telemetry | sub | 2015 | ongoing | Uncrewed | Civil | [26,328,329,330,331,332,333] |
| SAGITTA demonstrator | EA_0050 | Germany | P.P. | T&I | Flying Wing, Autonomous Jet | sub | 2014–2015 | 2020–2021 | Uncrewed | Civil | [26,328,329,330,331,332,333] |
| Flying V | EA_0051 | Germany | P.P. | T&I | Integrated BWB Airframe, Lightweight Composites | sub | 2014 2020 (first flight) | ongoing | Uncrewed | Civil | [334,335,336,337,338,339] |
| MOSUPS | EA_0052 | Poland | A.G. | T&I | Box-Wing Design, Ducted Fan Propulsion | sub | 2014 (first flight) | early 2020s (probably) | Uncrewed | Civil | [14,340,341,342,343,344] |
| TURAC | EA_0053 | Turkey | A.G. | T&I | Hybrid VTOL, Advanced Flight Control | sub | 2014 | ongoing | Uncrewed | Dual Use | [345,346,347] |
| Great Planes Avistar Elite | EA_0054 | USA | A.G. | R&E | Aerodynamic Simulation, Sensor Integration | sub | 2014 | ongoing | Uncrewed | Civil | |
| GL-10 Greased Lightning Prototype | EA_0055 | USA | P.G. | T&I | DEP, Tilt-Wing VTOL | sub | 2013 | 2017 | Crewed | Military | [348,349,350,351,352,353] |
| Technology- Evaluation Research Aircraft (PTERA) | EA_0056 | USA | P.P. | T&I | DEP, Autonomous Systems | sub | 2013 | ongoing | Uncrewed | Civil | [190,354,355] |
| UIUC Aero Testbed | EA_0057 | USA | A.G. | R&I | Electric Propulsion, Autonomous Control | sub | 2013 | possibly ongoing | Uncrewed | Civil | [41,356] |
| Sig Rascal 110 | EA_0058 | USA | A.G. | R&E | Large Airframe, Sensor Integration | sub | 2006 | possibly concluded | Uncrewed | Civil | [357,358,359] |
| Phastball | EA_0059 | USA | A.G. | R&E | EDF Propulsion, Autonomous Avionics | sub | around 2013 | possibly ongoing | Uncrewed | Civil | [360,361,362,363] |
| S3CM | EA_0060 | Japan | Public Governance | T&I | Low-Sonic-Boom Aero, Supersonic Control | sub | 2015 (first launch) | concluded-single use | Uncrewed | Civil | [31,364,365] |
| Yak-54 UAV | EA_0061 | USA | A.G. | R&I | Flight Control, Radar Sensors | sub | 2012 | possibly ongoing | Crewed | Civil | [366,367] |
| X-HALE | EA_0062 | USA | A.G | R&E | Flexible Wings, Aeroelastic Modeling | sub | 2010 | possibly ongoing | Uncrewed | Civil | [46,368,369,370] |
| Puffin demonstrator | EA_0063 | USA | P.G. | R&E | Tail-Sitter VTOL, Electric Propulsion | sub | 2008 | 2011 | Crewed | Civil | [33,371] |
| Hyperion 1.0, 2.0, 2.1 | EA_0064 | USA | A.G. | R&E | Hybrid Propulsion, BWB Design | sub | 2008 | 2011 | Uncrewed | Civil | [42,372,373] |
| Generic Future Fighter (GFF) demonstrator | EA_0065 | Sweeden | A.G. | R&E | Stealth, AI Autonomy, Advanced EW | full | 2009 | ongoing | Both crewed and uncrewed | Military | [374,375,376,377,378] |
| BB-1, BB-2, BB-3, BB-4 | EA_0066 | China | A.G. | T&I | BWB Aerodynamics, Low-Speed Dynamics | sub | 2008 | 2012 | Uncrewed | Civil | [3,379] |
| Raven | EA_0067 | Sweden | A.G. | R&E | Scaled Aircraft, Micro Turbines, Control Systems | sub | 2007 | possibly ongoing | Uncrewed | Civil | [3,45,380,381] |
| SensorCraft RPV | EA_0068 | USA | P.G. | T&I | SAR/EO Sensors, Stealth, Autonomous Flight | full | early 2000s | - | Uncrewed | Military | [382] |
| ECLIPSE | EA_0069 | UK | C.C. | T&I | Flapless (Fluidic) Control, Turbojet Propulsion | sub | 2009 2010 (first flight) | 2010 | Uncrewed | Defence–Military | [383,384,385,386,387] |
| VELA 2 | EA_0070 | Germany | A.G. | R&E | DEP, BWB Airframe | sub | 2007 | possibly concluded | Uncrewed | Civil | [50,388] |
| FASER (Ultrastick 120) | EA_0071 | USA | P.G. | T&I | Scaled Turbine Mode, Adaptive Control | sub | 2006 | ongoing | Uncrewed | Civil | [389,390] |
| GTM-T2 | EA_0072 | USA | P.G. | T&I | Flight Dynamics, System ID | sub | 2005 | finalized in 2010s | Uncrewed | Civil | [203,391,392,393] |
| Innovative Evaluation Platform (IEP) | EA_0073 | France | C.C. | T&I | Modular Testbed, Nonlinear Control | sub | 2005 | 2010 (NACRE project ending) | Uncrewed | Civil | [394,395,396,397] |
| AC20.30 | EA_0074 | Germany | A.G. | R&E | BWB, Scaled Electric Testbed | sub | early 2000s | possibly concluded | Uncrewed | Civil | [398] |
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| Research Methods |
|
| Data Sources (>390) |
|
| Analytical Framework |
|
| Geographic Scope | Europe (mainly) and Worldwide (international) |
| Temporal Scope | Past and Existing EA |
| Platform Types | Crewed and Uncrewed Vehicles |
| Application Scope | Civil and Defence Sectors |
| Number of EA identified | 74 |
| Key Attributes | Description | Key Attributes | Description |
|---|---|---|---|
| Testbed Name | Official name of the EA | Launch Year | Year operations started |
| ID No | Internal unique identifier for easy referencing | End of Operations Year | Year ended (if applicable) |
| Indicative Figure | A representative image or illustration of the EA | Main Organizations Involved | Partners or stakeholders |
| Country of Origin | Country where the testbed is based or coordinated | Crewed/Uncrewed | Type of aircraft or platform used |
| Governance Model/Leader Entity | Type of governance and lead organization | Civil/Defence–Military/Dual Use | Intended application or domain |
| Funding Structure/Main Funding | Source(s) of funding | Scale | Physical scale of the EA |
| Business Model | Operating approach | References | Source of the information (link, doc, partner input) |
| Key Testbed Technologies | Technologies tested |
| EA Name | Country of Origin | Governance Model | Funding Structure | Business Model | Launch Year |
|---|---|---|---|---|---|
| Clean Sky 2—SFD | Netherlands | Public Governance | Public Funding | Technology Demonstration and Strategic Innovation Business Model | 2017 |
| Airbus Flightlab-BLADE EA demonstrator | France | Public–Private partnership | Public–Private Funding | Technology Demonstration and Strategic Innovation Business Model | 2010 |
| General Electric Boeing 747-400 jumbo jet | USA | Corporate Governance | Private Funding | Technology Demonstration and Strategic Innovation Business Model | 2010 |
| Ilyushin Il-76 | Russia | Public Governance | Public Funding | Commercialization-focused | 1971 |
| e-Genius-Mod | Germany | Academic Governance | Public Funding | Technology Demonstration and Strategic Innovation Business Model | 2022 |
| GA-USTAR aircraft | USA | Academic Governance | Public Funding | Academic Research and Education | 2015 |
| Governance Model Type | Description | Representative EA Examples |
|---|---|---|
| Corporate Governance | This model is characterized by private ownership and control. A corporation or commercial entity is the primary decision-maker, overseeing the EA project in alignment with its business strategy, profitability goals, and shareholder interests. Governance is typically structured through formal corporate hierarchies, with executive leadership, boards of directors, and internal R&D units managing the initiative. This model is common in proprietary platforms developed for commercial product testing or technology demonstration. | Boeing ecoDemonstrator [15] Airbus UPNEXT [16] JetZero [17] |
| Public Governance | Public governance refers to EA that are wholly controlled and operated by governmental bodies or publicly funded research organizations. These testbeds are designed to serve national priorities, such as public safety, strategic capability development, or scientific advancement. Operations are fully funded through public budgets, with policy-driven decision-making, and often focus on civil aviation regulation, defence testing, or space research. | NASA X-57 Maxwell [18] NLR Research Aircraft Cessna Citation II [19] SWiFT (Stealth Wing Flying Testbed) [20] |
| Public–Private Partnership (PPP) | Under a PPP governance model, public sector entities (e.g., government agencies, national labs) and private companies collaborate to develop and operate the EA. Responsibilities, risks, and investments are shared, leveraging public oversight and objectives with private-sector innovation and efficiency. Decision-making structures are negotiated through formal agreements, often under joint steering committees or boards. PPPs are frequently used in dual-use or strategically significant testbeds. | Boeing X-48 [21] Rolls-Royce “Spirit of Innovation” [22] Kawasaki XC-2 [23] |
| Collaborative Consortium Governance | This model involves a network of multiple partners, often including universities, research institutions, private companies, and public agencies, working together through structured consortia. Decision-making is typically collective, based on consensus or shared governance bodies. This inclusive model supports joint innovation, open research, and distributed ownership, often aligned with EU-funded or multi-partner initiatives. | E-FAN X [24] H2FLY HY4 [25] ECLIPSE [25] |
| Academic Governance | In this structure, universities or academic institutions lead and operate the EA. The primary objectives centre around research, experimentation, education, and publication. Governance decisions are guided by academic leadership and faculty, often with funding from research grants and national or international research programs. These EA typically serve as open platforms for advancing early-stage or exploratory technologies. | UIUC Subscale Sukhoi [26] e-Genius-Mod [27] MOSUPS [14] |
| Funding Model Type | Description | Representative EA Examples |
|---|---|---|
| Private Funding | In this model, the EA is financed exclusively by private investors, including corporations, venture capitalists, or industry consortia. This model is driven primarily by commercial objectives, focusing on rapid innovation cycles, market-driven technology development, and potential financial returns. Private funding may offer greater operational agility but typically requires clear business models and demonstrable value propositions. | Alice Aircraft by Eviation [28] Vertical Aerospace [29] Diamond DA 62 [30] |
| Public Funding | In this model, financial support for the EA is provided entirely by government budgets or public grant programs. Funding is directed towards projects that serve broader societal or strategic goals such as advancing scientific knowledge, enhancing national security, or developing critical infrastructure. Public funding often ensures stable and long-term support but may be subject to political and budgetary constraints. | S3CM [31] GA-USTAR aircraft [32] Puffin demonstrator [33] |
| Public–Private Funding | This mixed funding structure combines resources from government entities and private sector participants. By sharing the financial burden, risks, and potential benefits, public–private funding models aim to leverage the strengths of both sectors: the public sector’s mandate for public interest and strategic investment, and the private sector’s drive for innovation and commercial viability. These partnerships often underpin testbeds with dual-use applications or significant technological challenges. | ZeroAvia Hydrogen Aircraft [34] MAGMA [35] Boeing ecoDemonstrator [15] |
| Business Model Type | Description | Representative EA Examples |
|---|---|---|
| Commercialization Focused | This model emphasizes transforming flying testbeds into revenue-generating products or services. The primary aim is to develop market-ready solutions that can be sold, licensed, or integrated through partnerships. Business success is measured by profitability, scalability, and market impact. Funding often involves private investment, and operations prioritize efficiency, customer needs, and commercial competitiveness. | Joby Aviation [36] Alice Aircraft by Eviation [28] Vertical Aerospace [29] |
| Technology Demonstration and Strategic Innovation | EA adopting this model are used to develop, validate, and showcase new aerospace technologies. Their purpose is to reduce technical and operational risks, provide proof of concept, and attract further investment or policy support. These testbeds often serve as platforms for early-stage innovation, enabling stakeholders to demonstrate capabilities that can lead to commercialization or regulatory adoption. | Airbus A350 XWB Testbed [37] Lockheed Martin CATBird [38] Boeing Phantom Ray [39] |
| Academic Research and Education | This business model centres on supporting scientific research and training the next generation of aerospace professionals. EA operating under this model primarily facilitate knowledge creation, curriculum development, and academic publication. Funding typically comes from research grants, public institutions, and educational programs. The focus is on exploration, experimentation, and contributing to the broader scientific community. | Cirrus SR22T [40] UIUC Aero Testbed [41] Hyperion 1.0–2.1 [42] |
| Aspects | USA | Europe |
|---|---|---|
| Dominant Governance | Public Governance (NASA, DoD) | Corporate (e.g., Airbus) |
| Corporate (Boeing, Lockheed, etc.) | Public–Private Partnerships (EU Frameworks) | |
| Funding | Public (NASA, DoD) | Public–Private (EU, Horizon 2020, national programs) |
| Public–Private (e.g., NASA-industry) | Corporate Investment | |
| Business Focus | Mixed: Aerospace/Defence (NASA, Lockheed) + Commercial eVTOL | Predominantly innovation-focused within Airbus and Rolls Royce |
| Academic Involvement | Strong (UIUC, MIT, etc.), many purely academic projects | Strong but more connected to EU consortia or applied research |
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© 2026 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license.
Share and Cite
Markatos, D.; Psihoyos, H.; Kalampoukas, T.; Iannelli, P.; Pellone, L.; Armbrust, M.; Strohmayer, A.; Pantelakis, S.; Filippatos, A. Experimental Aircraft: Comparative Analysis of Governance, Funding, and Business Models. Aerospace 2026, 13, 181. https://doi.org/10.3390/aerospace13020181
Markatos D, Psihoyos H, Kalampoukas T, Iannelli P, Pellone L, Armbrust M, Strohmayer A, Pantelakis S, Filippatos A. Experimental Aircraft: Comparative Analysis of Governance, Funding, and Business Models. Aerospace. 2026; 13(2):181. https://doi.org/10.3390/aerospace13020181
Chicago/Turabian StyleMarkatos, Dionysios, Harry Psihoyos, Thomas Kalampoukas, Pierluigi Iannelli, Lorenzo Pellone, Marco Armbrust, Andreas Strohmayer, Spiros Pantelakis, and Angelos Filippatos. 2026. "Experimental Aircraft: Comparative Analysis of Governance, Funding, and Business Models" Aerospace 13, no. 2: 181. https://doi.org/10.3390/aerospace13020181
APA StyleMarkatos, D., Psihoyos, H., Kalampoukas, T., Iannelli, P., Pellone, L., Armbrust, M., Strohmayer, A., Pantelakis, S., & Filippatos, A. (2026). Experimental Aircraft: Comparative Analysis of Governance, Funding, and Business Models. Aerospace, 13(2), 181. https://doi.org/10.3390/aerospace13020181

