About: Leonardo Next-Generation Civil Tiltrotor     Goto   Sponge   NotDistinct   Permalink

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The Leonardo Next-Generation Civil Tiltrotor (NextGenCTR or NGCTR) is a tiltrotor aircraft demonstrator designed and developed by the Italian aerospace company Leonardo S.p.A.Studies for a two times larger tiltrotor than the AgustaWestland AW609 started in 2000.Since 2014, its development is sponsored by the European Union's Clean Sky 2 program. By 2017, the maiden flight had been pushed back to 2023, from a 2020 initial plan.By May 2021, major components were under production

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  • Leonardo Next-Generation Civil Tiltrotor (en)
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  • The Leonardo Next-Generation Civil Tiltrotor (NextGenCTR or NGCTR) is a tiltrotor aircraft demonstrator designed and developed by the Italian aerospace company Leonardo S.p.A.Studies for a two times larger tiltrotor than the AgustaWestland AW609 started in 2000.Since 2014, its development is sponsored by the European Union's Clean Sky 2 program. By 2017, the maiden flight had been pushed back to 2023, from a 2020 initial plan.By May 2021, major components were under production (en)
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  • http://commons.wikimedia.org/wiki/Special:FilePath/Leonardo_Next-Generation_Civil_Tiltrotor.png
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  • met (en)
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  • planned 2023 (en)
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  • May 2022 (en)
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  • CleanSky goals are 30-50% lower costs, not "similar" (en)
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  • Flightglobal (en)
related
  • * AgustaWestland AW609 (en)
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  • Under development (en)
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  • Tiltrotor demonstrator (en)
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  • The Leonardo Next-Generation Civil Tiltrotor (NextGenCTR or NGCTR) is a tiltrotor aircraft demonstrator designed and developed by the Italian aerospace company Leonardo S.p.A.Studies for a two times larger tiltrotor than the AgustaWestland AW609 started in 2000.Since 2014, its development is sponsored by the European Union's Clean Sky 2 program. By 2017, the maiden flight had been pushed back to 2023, from a 2020 initial plan.By May 2021, major components were under production The 11 t (24,000 lb) MTOW, pressurised aircraft should seat 19 to 22 passengers, reach up to 330 kn (610 km/h) over a range of 500 nmi (930 km).Initial requirements targeted lower costs than conventional rotorcraft.The engines stay in a fixed position while the proprotors swivels independently, powered by a split gearbox. (en)
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  • turboshaft engines (en)
lists
  • * List of VTOL aircraft (en)
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  • Y (en)
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see also
  • * Airbus RACER (en)
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