Английская Википедия:Hexadyne P60

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Шаблон:Short description Шаблон:Use mdy dates Шаблон:Use American English

The Hexadyne P60 is an American aircraft engine, designed and produced by Hexatron Engineering of Salt Lake City, Utah for use in ultralight and homebuilt aircraft.[1]

Design and development

The engine is a twin cylinder four-stroke, horizontally-opposed, Шаблон:Convert, air-cooled, gasoline engine design, with a mechanical gearbox spur gear reduction drive with a reduction ratio of 2.5:1. It employs electronic ignition and produces Шаблон:Convert continuous at 5750 rpm. The engine management system is a six-sensor computer and the engine is optimized to drive a Шаблон:Convert propeller.[1][2]

The engine was initially displayed at AirVenture, Oshkosh, Wisconsin in 2001.[2]

Applications

Specifications (Hexadyne P60)

Шаблон:Pistonspecs

See also

Шаблон:Aircontent

References

Шаблон:Reflist

External links

  1. 1,0 1,1 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 238-241. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. 2,0 2,1 Шаблон:Cite web
  3. Шаблон:Cite web