ENSIKLOPEDIA Cari Tekan Enter untuk memulai pencarian cepat. Kembali ke Ensiklopedia Arsip Wikipedia Indonesia Rotax 275 Rotax 275Austrian two-stroke aircraft engine 275TypePiston aero-engineNational originAustriaManufacturerRotaxMajor applicationsSelf-launching Gliders] 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] 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.[1] Applications Glaser-Dirks DG-600M Schleicher ASH 25E Schleicher ASW 24E Specifications (275) Data from EASA Type Certificate[1] General characteristicsType: 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 PerformancePower output: 17.6 kW (26 hp) at 7000 L/min References 1 2 3 EASA Type-Certificate Data Sheet No E.210 for Rotax 275 series engines (Issue 03 Dated 5 September 2016) vteRotax aircraft enginesTwo-stroke piston engines 185 275 277 377 447 462 503 532 535 582 618 Four-stroke piston engines 912 914 915 916