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The Rotax 532 is a 48 kW (64 hp) two-stroke, two-cylinder, rotary valve engine, liquid-cooled, gear reduction-drive engine that was formerly manufactured by BRP-Rotax GmbH & Co. KG. It was designed for use on ultralight aircraft.
, Der Rotax 532 ist ein wassergekühlter Zweizylinder-Zweitakt-Flugzeugreihenmotor mit einer Leistung von 48 kW (65 PS) und Drehventilen. Er wurde von der österreichischen Firma BRP-Rotax als Triebwerk für Ultraleichtflugzeuge gebaut.
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22025911
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4392
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1091709479
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| http://dbpedia.org/property/bore
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72.0
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| http://dbpedia.org/property/coolingsystem
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liquid cooled
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| http://dbpedia.org/property/displacement
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521.2
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| http://dbpedia.org/property/fueltype
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premium unleaded: RON 90 octane or higher leaded or unleaded or AVGAS 100 LL
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http://dbpedia.org/resource/Rotax +
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http://dbpedia.org/resource/Austria +
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| http://dbpedia.org/property/oilsystem
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oil-in-fuel at 50:1
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| http://dbpedia.org/property/power
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48
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| http://dbpedia.org/property/power/weight
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0.62
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| http://dbpedia.org/property/stroke
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64.0
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| http://dbpedia.org/property/type
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http://dbpedia.org/resource/Aircraft_engine +
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, 2
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| http://dbpedia.org/property/valvetrain
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rotary inlet valve, piston ported exhaust
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| http://dbpedia.org/property/weight
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46.8
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| rdfs:comment |
Der Rotax 532 ist ein wassergekühlter Zweizylinder-Zweitakt-Flugzeugreihenmotor mit einer Leistung von 48 kW (65 PS) und Drehventilen. Er wurde von der österreichischen Firma BRP-Rotax als Triebwerk für Ultraleichtflugzeuge gebaut.
, The Rotax 532 is a 48 kW (64 hp) two-stroke, two-cylinder, rotary valve engine, liquid-cooled, gear reduction-drive engine that was formerly manufactured by BRP-Rotax GmbH & Co. KG. It was designed for use on ultralight aircraft.
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| rdfs:label |
Rotax 532
|
