The Rotax 275 is a 24 hp (18 kW), single-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in Self-launched Gliders.[1]
| 275 | |
|---|---|
| Type | Piston aero-engine |
| National origin | Austria |
| Manufacturer | Rotax |
| Major applications | Self-launching Gliders] |
Design edit
The Rotax 275 is a single-cylinder two-stroke engine with an air-cooled cylinder head and cylinder. It has a single magneto ignition with a gear driven propeller. It was certified in Austria in November 1988.[1]
Applications edit
Specifications (275) edit
Data from EASA Type Certificate[1]
General characteristics
- Type: two-stroke air-cooled aeroengine
- Bore: 72 mm (2.83 in)
- Stroke: 66 mm (2.60 in)
- Displacement: 268.7 cc (16.40 cu in)
- Dry weight: 25 kg (complete with muffler and starter)
Components
- Fuel type: two-stroke mixture
- Cooling system: free air
Performance
- Power output: 17.6 kW (26 hp) at 7000 L/min
References edit