Matches in DBpedia 2014 for { <http://dbpedia.org/resource/Rotax_618> ?p ?o. }
Showing items 1 to 32 of
32
with 100 items per page.
- Rotax_618 abstract "The Rotax 618 is a 73.8 hp (55 kW) two-stroke, two-cylinder, liquid cooled, gear reduction-drive engine that was formerly manufactured by BRP-Rotax GmbH & Co. KG. It was designed for use on ultralight aircraft.".
- Rotax_618 thumbnail MurphyRenegadeSpiritC-IDBK.JPG?width=300.
- Rotax_618 wikiPageID "22026197".
- Rotax_618 wikiPageRevisionID "604612308".
- Rotax_618 bore "76.0".
- Rotax_618 coolingsystem "liquid cooled".
- Rotax_618 displacement "617.0".
- Rotax_618 fueltype "premium unleaded: RON 90 octane or higher leaded or unleaded or AVGAS 100 LL".
- Rotax_618 hasPhotoCollection Rotax_618.
- Rotax_618 majorApplications Blue_Yonder_Merlin.
- Rotax_618 majorApplications Murphy_Renegade.
- Rotax_618 manufacturer Rotax.
- Rotax_618 nationalOrigin Austria.
- Rotax_618 oilsystem "oil-in-fuel at 50:1".
- Rotax_618 power "55".
- Rotax_618 weight "0.56".
- Rotax_618 stroke "68.0".
- Rotax_618 type Aircraft_engine.
- Rotax_618 type Piston.
- Rotax_618 type "2".
- Rotax_618 valvetrain "rotary inlet valve, exhaust valve".
- Rotax_618 weight "59.1".
- Rotax_618 subject Category:Rotax_engines.
- Rotax_618 subject Category:Two-stroke_aircraft_piston_engines.
- Rotax_618 comment "The Rotax 618 is a 73.8 hp (55 kW) two-stroke, two-cylinder, liquid cooled, gear reduction-drive engine that was formerly manufactured by BRP-Rotax GmbH & Co. KG. It was designed for use on ultralight aircraft.".
- Rotax_618 label "Rotax 618".
- Rotax_618 sameAs m.05pb8p8.
- Rotax_618 sameAs Q7370344.
- Rotax_618 sameAs Q7370344.
- Rotax_618 wasDerivedFrom Rotax_618?oldid=604612308.
- Rotax_618 depiction MurphyRenegadeSpiritC-IDBK.JPG.
- Rotax_618 isPrimaryTopicOf Rotax_618.
