Rotax 275
# Rotax 275

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.

## Design

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.

## Applications

* Glaser-Dirks DG-600M
* Schleicher ASH 25E
* Schleicher ASW 24E

## Specifications (275)

Data from EASA Type Certificate

### 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
