Raven 1300 SVS Turbo

1300 SVS Turbo
Type Aircraft engine
National origin United States
Manufacturer Raven Redrives
Unit cost US$10,950 (2015)

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]

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. 1 2 3 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. 1 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.
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