Raven 1300 SVS Turbo

The Raven 1300 SVS Turbo is an American aircraft engine, designed and produced by Raven Redrives of El Prado, New Mexico for use in ultralight and homebuilt aircraft.[1][2]

1300 SVS Turbo
Type Aircraft engine
National origin United States
Manufacturer Raven Redrives

The company seems to have gone out of business in 2017 and production ended.[3]

Design and development

The engine is a turbocharged four-cylinder four-stroke, in-line, 1,300 cc (79.3 cu in) displacement, liquid-cooled, automotive conversion, gasoline engine design, with a poly V belt reduction drive with a reduction ratio of 2.11:1. It employs electronic ignition and produces 115 hp (86 kW) at 5700 rpm.[1]

A normally-aspirated version was also built, producing 90 hp (67 kW).[2]

Specifications (1300 SVS Turbo)

Data from Tacke[1]

General characteristics

  • Type: Four cylinder, four stroke, turbocharged aircraft engine
  • Bore: 74 mm (2.9 in)
  • Stroke: 77 mm (3.0 in)
  • Displacement: 1,300 cc (79.3 cu in)
  • Dry weight: 80 kg (176.4 lb)

Components

  • Fuel type: gasoline
  • Cooling system: liquid
  • Reduction gear: poly V belt

Performance

  • Power output: 115 hp (86 kW)

See also

Related lists

References
  1. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. Raven Redrives. "Geo Metro/Suzuki Auto Engine Conversions". www.raven-rotor.com. Archived from the original on 9 April 2018. Retrieved 8 April 2018.
  3. "Internet Archive Wayback Machine". archive.org. Retrieved 8 April 2018.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.