RED A03

The RED A03 is a V12 four-stroke aircraft diesel engine designed and built by RED Aircraft GmbH of Adenau, Germany.[1]

A03
RED A03 V-12 engine
Type Aircraft diesel engine
National origin Germany
Manufacturer RED Aircraft GmbH
First run 2009
RED A03 installed in a Yakovlev Yak-52

Development

In 2012, its unit cost was US$170,000.[2] 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.[1] It powered the Yakovlev Yak-152 trainer on its 29 September 2016 first flight.[3] The RED A03 is presented by the ILA Berlin Air Show as an application in the Aerobatic sector and for Defence and Security.[4] 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.[5]

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.[6] RED Aircraft is a member of The German Aerospace Industry Association,[7] itself a member of the International Astronautical Federation.[8]

Design

It has twin double overhead camshafts. A marine version was planned for 522 kW/700 hp at 3,900 rpm.[9] The cylinder banks' angle is 80 degrees [10] It was designed by Vladimir Raikhlin, a German engineer born in Russia.

Applications

Specifications

Data from EASA Type-Certificate Data Sheet[1]

General characteristics

  • Type: four-stroke compression-ignition piston engine
  • Bore: 86mm[15]
  • Stroke: 88m[15]
  • Displacement: 6134 cc
  • Length: 1100 mm
  • Width: 850 mm
  • Height: 750 mm
  • Dry weight: 363 kg (RED A03-003), 357 kg (RED A03-102) dry

Components

Performance

  • Power output: 368kW (500 HP)Take-off at 2127 propeller rpm; 338kW (460 HP) maximum continuous at 1995 Propeller RPM
  • Specific fuel consumption: 210 g/kW/h (0.35 lb/hp/h) at 400 hp, 1862 prop. RPM, sea level[15]

RED A05 300hp V6

The RED A05 is a 2017 preliminary design of a V6 engine with 3,550 cc (217 cu in) displacement, outputting 300 hp (220 kW) at takeoff at 2127 propeller RPM and 280 hp (210 kW) continuously at 1995 propeller RPM, with a 210 g/kW/h (0.35 lb/hp/h) best brake specific fuel consumption.[16]

See also

References

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