|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:light_aircraft
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:compression_ratio
|
8.5:1
|
|
gptkbp:configuration
|
inline-four
|
|
gptkbp:control_system
|
electronic fuel injection
|
|
gptkbp:cooling_system
|
liquid-cooled
liquid and air cooled
|
|
gptkbp:displacement
|
1,200 cc
|
|
gptkbp:engine_type
|
turbocharged
|
|
gptkbp:first_introduced
|
1990s
|
|
gptkbp:fuel_capacity
|
approximately 600 mm
4.5 L
approximately 500 mm
approximately 400 mm
|
|
gptkbp:fuel_economy
|
approximately 30 L/h
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rotax 914
|
|
gptkbp:ignition_system
|
gptkb:4
dual ignition
|
|
gptkbp:is_often_used_in
|
ultralight aircraft
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
gptkb:BRP-Rotax
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:max_speed
|
5,800 RPM
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:powers
|
100 hp
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:related_aircraft
|
gptkb:Aero_AT-3
gptkb:Boeing_707
gptkb:Pipistrel_Alpha_Trainer
gptkb:Cessna_162
gptkb:Aerospool_WT9
gptkb:Diamond_DA20
gptkb:Aero_AT-4
gptkb:Aero_Vodochody_L-159
gptkb:Aero_Vodochody_L-39
gptkb:Aero_Vodochody_L-39_Albatros
gptkb:Aero_Vodochody_L-39_C
gptkb:Aero_Vodochody_L-39_ZA
gptkb:Aero_Vodochody_L-59
gptkb:Evektor_Sport_Star
gptkb:Flight_Design_CT
gptkb:Pipistrel_Virus
gptkb:Rans_S-6
gptkb:Tecnam_P92
gptkb:Zenith_CH_701
Skyboy
|
|
gptkbp:torque
|
120 Nm
|
|
gptkbp:type
|
four-stroke engine
|
|
gptkbp:valve_configuration
|
DOHC
|
|
gptkbp:weight
|
approximately 70 kg
|
|
gptkbp:bfsParent
|
gptkb:MQ-1_Predator
|
|
gptkbp:bfsLayer
|
4
|