Ultimate PROJECT

This project has received funding from the European Union's Horizon 2020 research and innovation programme under agreement No 633436

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  • ULTIMATE Technologies
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    • Results overview
    • Intercooled core with pulsed detonation combustion for intra-European missions
    • Intercooled geared turbofan with pulsed detonation combustion for Intercontinental missions
    • Open rotor with a nutating-disc topping cycle
    • Turbofan with a closed-circuit bottoming cycle
    • Turbofan with topping and bottoming cycles
    • Ultra-thin Adaptive Inlet Concept
    • Secondary Fluid Recuperator (SFR) concept
    • Composite Cycle Engine (CCE)
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  • Ultra Low emission Technology Innovations for Mid-century Aircraft Turbine Engines
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  • News & Events
  • Press and communication Material
  • Available Documentation
  • Scientific Publications

Partners

Chalmers Tekniska Hoegskola AB
Aristotle University of Thessaloniki
Cranfield University
Institut supérieur de l'aéronautique et de l'espace
Bauhaus Luftfahrt e.V.
GKN Aerospace Sweden AB
MTU Aero Engines AG
Rolls-Royce plc
Safran Aircraft Engines
ARTTIC
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Ultimate Project

This project has received funding from the European Union's Horizon 2020 research and innovation programme under agreement No 633436

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  • About
  • ULTIMATE Technologies
  • Partners
  • Results
  • Media Center
  • Useful Links
  • Contact