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Red engine 3
Red engine 3










red engine 3 red engine 3

  • Power output: 368kW (500 HP)Take-off at 2127 propeller rpm 338kW (460 HP) maximum continuous at 1995 Propeller RPM.
  • Fuel type: jet-fuel, kerosene-type/diesel.
  • Type: four-stroke compression-ignition piston engine.
  • Russian unmanned combat aerial vehicle Altair/Altius prototype ĭata from EASA Type-Certificate Data Sheet General characteristics.
  • In-development twin-engine utility aircraft for 9-14 passengers or cargo from Russian Pro-Avia.
  • Yakovlev Yak-52 and Yakovlev Yak-152 trainers.
  • Otto Celera 500L (experimental civil utility and executive transport aircraft).
  • Hybrid Air Vehicles HAV 304/Airlander 10 (proposed).
  • De Havilland Canada DHC-2 Beaver (STC planned).
  • It was designed by Vladimir Raikhlin, a German engineer born in Russia. A marine version was planned for 522 kW/700 hp at 3,900 rpm. RED Aircraft is a member of The German Aerospace Industry Association, itself a member of the International Astronautical Federation. On 30 March 2020, RED Aircraft received a certificate of aerospace quality management system standard EN 9100:2018, based on ISO 9001:2015, from AirCert.

    red engine 3

    The engine is proposed for the Hybrid Air Vehicles HAV 304/Airlander 10, a British hybrid airship design, powered by four engines and can be operated with two. The RED A03 is presented by the ILA Berlin Air Show as an application in the Aerobatic sector and for Defence and Security. It powered the Yakovlev Yak-152 trainer on its 29 September 2016 first flight. The engine received type approval from the European Aviation Safety Agency in December 2014 for use in any CS-23 aircraft in both normal and utility categories.












    Red engine 3