Rotax 912 ULS

GPTKB entity

Statements (29)
Predicate Object
gptkbp:instanceOf 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
https://www.w3.org/2000/01/rdf-schema#label Rotax 912 ULS
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
light sport aircraft
gptkbp:valveConfiguration 8 valves
gptkbp:weight 63.6 kg
gptkbp:bfsParent gptkb:Zlin_Aviation_Shock_Ultra
gptkbp:bfsLayer 6