Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
84 mm
|
| gptkbp:certification |
non-certified (ULS version)
|
| gptkbp:compressionRatio |
10.5:1
|
| gptkbp:coolingSystem |
liquid-cooled cylinder heads
air-cooled cylinders |
| gptkbp:countryOfOrigin |
gptkb:Austria
|
| gptkbp:displacement |
1352 cc
|
| gptkbp:engineType |
four-stroke
|
| gptkbp:family |
Rotax 912 series
|
| gptkbp:fuelType |
avgas
carbureted mogas ~15-20 L/h at cruise |
| gptkbp:gearbox |
integrated
|
| gptkbp:ignition |
dual electronic ignition
|
| gptkbp:introduced |
1999
|
| gptkbp:manufacturer |
gptkb:Rotax
|
| gptkbp:maximumSpeed |
5800 rpm
|
| gptkbp:numberOfEngines |
4
|
| gptkbp:powerOutput |
100 hp
|
| gptkbp:stroke |
61 mm
|
| gptkbp:usedIn |
gptkb:aircraft
gptkb:light_sport_aircraft |
| gptkbp:valveConfiguration |
8 valves
|
| gptkbp:weight |
63.6 kg
|
| gptkbp:bfsParent |
gptkb:Rotax_engines
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rotax 912 ULS
|