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)
Performance
- Power output: 115 hp (86 kW)
References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Raven Redrives. "Geo Metro/Suzuki Auto Engine Conversions". www.raven-rotor.com. Archived from the original on 9 April 2018. Retrieved 8 April 2018.
- "Raven Rotor". Internet Archive Wayback Machine. Retrieved 8 April 2018.
External links
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