|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:certification
|
gptkb:ASTM_F2339
gptkb:EASA_CS-22
gptkb:EASA_CS-LSA
|
|
gptkbp:compressionRatio
|
9.1:1
|
|
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
15-20 liters/hour
automotive gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rotax 912
|
|
gptkbp:ignition
|
dual electronic ignition
|
|
gptkbp:manufacturer
|
gptkb:Rotax
gptkb:BRP-Rotax_GmbH_&_Co_KG
|
|
gptkbp:marketedAs
|
gptkb:BRP-Rotax
|
|
gptkbp:maximumSpeed
|
5,800 rpm
|
|
gptkbp:notableAircraft
|
gptkb:Cessna_162_Skycatcher
gptkb:Tecnam_P92
gptkb:Zenith_CH_601
gptkb:Evektor_SportStar
gptkb:Flight_Design_CT
gptkb:Pipistrel_Virus
gptkb:Diamond_DA20
gptkb:Aeroprakt_A-22
gptkb:Remos_GX
|
|
gptkbp:oilSystem
|
dry sump
|
|
gptkbp:powerOutput
|
100 hp
80 hp
|
|
gptkbp:propulsion
|
geared reduction drive
|
|
gptkbp:relatedTo
|
gptkb:Rotax_914
gptkb:Rotax_912_iS
|
|
gptkbp:usedIn
|
gptkb:aircraft
light sport aircraft
gyrocopters
|
|
gptkbp:valveConfiguration
|
8 valves
|
|
gptkbp:variant
|
gptkb:Rotax_912_A
gptkb:Rotax_912_F
gptkb:Rotax_912_S
gptkb:Rotax_912_UL
gptkb:Rotax_912_ULS
|
|
gptkbp:weight
|
56.6 kg
|
|
gptkbp:bfsParent
|
gptkb:Flight_Design_CTSL
gptkb:Zlin_Aviation_Savage_Cub
gptkb:Zlin_Aviation_Savage_Shock_Ultra
gptkb:Zlin_Savage_Cub
gptkb:Bayraktar_TB2_drone
gptkb:Bayraktar_TB2
gptkb:E-AC-3
|
|
gptkbp:bfsLayer
|
6
|