Raven 1300 SVS Turbo
From Wikipedia, the free encyclopedia
| 1300 SVS Turbo | |
|---|---|
| Type | Aircraft engine |
| National origin | United States |
| Manufacturer | Raven Redrives |
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]
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)