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Active HORIZON European Commission

COMmon Platform and Advanced INstrumentation ReadIness for ultra efficient propulsion demonstratiON

€25.9M EUR

Funder European Commission
Recipient Organization Airbus Operations Sas
Country France
Start Date Jan 01, 2024
End Date Jun 30, 2026
Duration 911 days
Number of Grantees 14
Roles Third Party; Participant; Coordinator; Associated Partner
Data Source European Commission
Grant ID 101140627
Grant 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%.

All Grantees

Airbus; Stichting Duits-Nederlandse Windtunnels; Stichting Koninklijk Nederlands Lucht - En Ruimtevaartcentrum; Insavalor Sa; Airbus Operations Sas; Centrale Innovation Sa; Institut National Des Sciences Appliquees de Lyon; Office National D'Etudes Et de Recherches Aerospatiales; Deutsches Zentrum Fur Luft - Und Raumfahrt Ev; Easn Technology Innovation Services Bvba; Airbus Operations Limited; Airbus Operations Gmbh; Airbus Operations Sl; Ecole Centrale de Lyon

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