Hexadyne P60
Type Aircraft engine
National origin United States
Manufacturer Hexatron Engineering Co., Inc.

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, 800 cc (48.8 cu in), 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 60 hp (45 kW) continuous at 5750 rpm. The engine management system is a six-sensor computer and the engine is optimized to drive a 68 to 70 in (173 to 178 cm) propeller.[1][2]

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

Applications

Specifications (Hexadyne P60)

Data from World Directory of Leisure Aviation 2011-12[1] and manufacturer[2]

General characteristics

  • Type: Twin cylinder, four-stroke aircraft engine
  • Bore: 92 mm (3.6 in)
  • Displacement: 800 cc (48.8 cu in)
  • Length: 596 mm (23.5 in)
  • Width: 406 mm (16.0 in)
  • Height: 450 mm (17.7 in)
  • Dry weight: 45 kg (99.2 lb)

Components

Performance

  • Power output: 60 hp (45 kW) at 5750 rpm
  • Compression ratio: 9.0:1
  • Fuel consumption: 3 U.S. gallons (11 L; 2.5 imp gal) per hour

See also

Related lists

References

  1. 1 2 3 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. 1 2 3 "Hexatron Product 2". hexatronengineering.com. Retrieved July 14, 2015.
  3. ↑ "Hexadyne P60 Fire Wall Mounting". Hexatron Engineering. Archived from the original on July 5, 2015. Retrieved July 15, 2015.
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