Rotax 912 engine

GPTKB entity

Statements (30)
Predicate Object
gptkbp:instanceOf piston engine
gptkbp:category piston aircraft engine
gptkbp:compressionRatio 9.1:1
gptkbp:configuration horizontally opposed
gptkbp:coolingSystem liquid-cooled cylinder heads
air-cooled cylinders
gptkbp:countryOfOrigin gptkb:Austria
gptkbp:displacement 1,211 cc
gptkbp:engineType four-stroke
flat-four
gptkbp:firstFlight 1989
gptkbp:fuelType aviation gasoline
automotive gasoline
https://www.w3.org/2000/01/rdf-schema#label Rotax 912 engine
gptkbp:ignition dual electronic ignition
gptkbp:manufacturer gptkb:Rotax
gptkb:BRP-Rotax_GmbH_&_Co_KG
gptkbp:numberOfEngines 4
gptkbp:powerOutput 100 hp
80 hp
gptkbp:propulsion geared reduction drive
gptkbp:relatedTo Rotax 912 S engine
Rotax 912 iS engine
Rotax 914 engine
gptkbp:usedIn gptkb:aircraft
light sport aircraft
gyrocopters
gptkbp:weight 56 kg
gptkbp:bfsParent gptkb:TB2
gptkbp:bfsLayer 7