Rotax 914 four-cylinder engine
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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
|
| 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:MQ-1_Predator
gptkb:Predator_drone |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rotax 914 four-cylinder engine
|