Summary
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The purpose of the COMPANION project is to define, design and prepare a common flight test demonstrator platform to enable the validation of ultra-efficient propulsion systems developed in Clean Aviation Call#01 projects at full scale and in a wide envelope of realistic operational conditions.
Given the clear requirement in the roadmap planning of the CA projects OFELIA and SWITCH for flight test demonstrations in Clean Aviation Phase 2 to achieve TRL 6 before the end of the program in 2030, a corresponding platform must be prepared to be available before the end of year 2026.
The project targets to prepare and deliver the hardware of the flight test platform ready for engine installation by the end of June 2026. The flight clearance process will be opened in COMPANION, but will need to continue with the installation of the demonstrator engines in follow-up projects to be defined at the end of CA Phase 1.
The project plan proposes to prepare a common flight test demonstrator platform on the basis of an Airbus A380 aircraft with one of the inboard engine pylons modified to accommodate versatile ultra-efficient proposal systems which are currently under development for a Clean Aviation Short Range and Short and Medium Range concept aircraft, namely an Open Rotor test engine and a hybrid electric Ultra High ByPass Turbofan. The flight test aircraft will be fully equipped to host a diversity of standard and special flight test instrumentation that will be defined in close cooperation with the projects OFELIA and SWITCH to provide all data required to quantify the performance of the demonstrator engines under operational conditions. The test aircraft allows the demonstrator engines to operate on conventional kerosene and SAF fuel at blending rates of up to 100%.
"
The purpose of the COMPANION project is to define, design and prepare a common flight test demonstrator platform to enable the validation of ultra-efficient propulsion systems developed in Clean Aviation Call#01 projects at full scale and in a wide envelope of realistic operational conditions.
Given the clear requirement in the roadmap planning of the CA projects OFELIA and SWITCH for flight test demonstrations in Clean Aviation Phase 2 to achieve TRL 6 before the end of the program in 2030, a corresponding platform must be prepared to be available before the end of year 2026.
The project targets to prepare and deliver the hardware of the flight test platform ready for engine installation by the end of June 2026. The flight clearance process will be opened in COMPANION, but will need to continue with the installation of the demonstrator engines in follow-up projects to be defined at the end of CA Phase 1.
The project plan proposes to prepare a common flight test demonstrator platform on the basis of an Airbus A380 aircraft with one of the inboard engine pylons modified to accommodate versatile ultra-efficient proposal systems which are currently under development for a Clean Aviation Short Range and Short and Medium Range concept aircraft, namely an Open Rotor test engine and a hybrid electric Ultra High ByPass Turbofan. The flight test aircraft will be fully equipped to host a diversity of standard and special flight test instrumentation that will be defined in close cooperation with the projects OFELIA and SWITCH to provide all data required to quantify the performance of the demonstrator engines under operational conditions. The test aircraft allows the demonstrator engines to operate on conventional kerosene and SAF fuel at blending rates of up to 100%.
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More information & hyperlinks
| Web resources: | https://cordis.europa.eu/project/id/101140627 |
| Start date: | 01-01-2024 |
| End date: | 30-06-2026 |
| Total budget - Public funding: | 25 904 176,50 Euro - 19 947 000,00 Euro |
Cordis data
Original description
"The purpose of the COMPANION project is to define, design and prepare a common flight test demonstrator platform to enable the validation of ultra-efficient propulsion systems developed in Clean Aviation Call#01 projects at full scale and in a wide envelope of realistic operational conditions.
Given the clear requirement in the roadmap planning of the CA projects OFELIA and SWITCH for flight test demonstrations in Clean Aviation Phase 2 to achieve TRL 6 before the end of the program in 2030, a corresponding platform must be prepared to be available before the end of year 2026.
The project targets to prepare and deliver the hardware of the flight test platform ready for engine installation by the end of June 2026. The flight clearance process will be opened in COMPANION, but will need to continue with the installation of the demonstrator engines in follow-up projects to be defined at the end of CA Phase 1.
The project plan proposes to prepare a common flight test demonstrator platform on the basis of an Airbus A380 aircraft with one of the inboard engine pylons modified to accommodate versatile ultra-efficient proposal systems which are currently under development for a Clean Aviation Short Range and Short and Medium Range concept aircraft, namely an Open Rotor test engine and a hybrid electric Ultra High ByPass Turbofan. The flight test aircraft will be fully equipped to host a diversity of standard and special flight test instrumentation that will be defined in close cooperation with the projects OFELIA and SWITCH to provide all data required to quantify the performance of the demonstrator engines under operational conditions. The test aircraft allows the demonstrator engines to operate on conventional kerosene and SAF fuel at blending rates of up to 100%.
"
Status
SIGNEDCall topic
HORIZON-JU-CLEAN-AVIATION-2023-02-SMR-01Update Date
12-03-2024
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Organisations
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| Airbus Operations SAS (Coördinator)
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| AIRBUS
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| AIRBUS OPERATIONS LIMITED
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| AIRBUS OPERATIONS SL
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| Airbus Operations GmbH
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| CENTRALE INNOVATION SA
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| DEUTSCHES ZENTRUM FUR LUFT - UND RAUMFAHRT EV
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| EASN TECHNOLOGY INNOVATION SERVICES BVBA
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| ECOLE CENTRALE DE LYON
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| INSAVALOR SA
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| INSTITUT NATIONAL DES SCIENCES APPLIQUEES DE LYON
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| OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES (ONERA)
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| STICHTING DUITS-NEDERLANDSE WINDTUNNELS
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| Stichting Nationaal Lucht- En Ruimtevaartlaboratorium (NLR - Royal Netherlands Aerospace Centre)