Rotax 914 four-cylinder engine
GPTKB entity
Statements (23)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:application |
gptkb:aircraft
|
gptkbp:certification |
gptkb:FAA
gptkb:EASA_CS-E |
gptkbp:compressionRatio |
9.0:1
|
gptkbp:coolingSystem |
air-cooled
liquid-cooled cylinder heads |
gptkbp:displacement |
1211 cc
|
gptkbp:engineType |
horizontally opposed
four-cylinder |
gptkbp:fuelType |
gptkb:gasoline
|
https://www.w3.org/2000/01/rdf-schema#label |
Rotax 914 four-cylinder engine
|
gptkbp:ignition |
dual electronic ignition
|
gptkbp:introduced |
1996
|
gptkbp:manufacturer |
gptkb:BRP-Rotax
|
gptkbp:powerOutput |
115 hp
|
gptkbp:propulsion |
geared reduction drive
|
gptkbp:turbocharged |
yes
|
gptkbp:weight |
72.6 kg
|
gptkbp:bfsParent |
gptkb:RQ-1_Predator
gptkb:MQ-1_Predator gptkb:Predator_drone |
gptkbp:bfsLayer |
6
|