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] 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] Data from EASA Type Certificate[1]