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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
|
gptkb:light_aircraft
|
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gptkbp:certification
|
certified by EASA
|
|
gptkbp:compression_ratio
|
10.5:1
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|
gptkbp:configuration
|
flat-four
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gptkbp:control_system
|
ECU
|
|
gptkbp:cooling_system
|
liquid-cooled
air-cooled and liquid-cooled
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|
gptkbp:cylinder_bore
|
100 mm
|
|
gptkbp:cylinder_stroke
|
82 mm
|
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gptkbp:displacement
|
912 cc
|
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gptkbp:emissions_standard
|
EURO 4
|
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gptkbp:enforces
|
compliant with EASA regulations
|
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gptkbp:engine
|
gptkb:light_aircraft
electric start
dual ignition system
ultralight aircraft
100 hp at 5800 RPM
|
|
gptkbp:engine_configuration
|
modular design
horizontally opposed
flexible mount
|
|
gptkbp:engine_power
|
high performance
high reliability
75 k W
popular in aviation community
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|
gptkbp:engine_type
|
gptkb:912i_S_Sport
reciprocating engine
|
|
gptkbp:first_introduced
|
gptkb:2012
|
|
gptkbp:fuel_capacity
|
500 mm
600 mm
400 mm
4.5 L
132 lbs
|
|
gptkbp:fuel_economy
|
high fuel efficiency
|
|
gptkbp:fuel_type
|
aviation gasoline
electronic fuel injection
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rotax 912i S
|
|
gptkbp:ignition_system
|
gptkb:NGK
dual ignition
|
|
gptkbp:is_tested_for
|
extensively tested
|
|
gptkbp:maintenance
|
low maintenance
|
|
gptkbp:manufacturer
|
gptkb:BRP-Rotax
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:max_speed
|
5800 RPM
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:power_output
|
100 hp
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:service_frequency
|
200 hours
|
|
gptkbp:torque
|
120 Nm
88 lb-ft
|
|
gptkbp:type
|
four-stroke engine
|
|
gptkbp:valve_configuration
|
SOHC
|
|
gptkbp:weight
|
60 kg
|
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gptkbp:bfsParent
|
gptkb:Rotax_912_S
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gptkbp:bfsLayer
|
6
|