Rolls-Royce AE 1107C-Liberty
GPTKB entity
Properties (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboshaft engine
|
| gptkbp:compressionRatio |
16:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
600 mm
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:engineConfiguration |
twin-spool
|
| gptkbp:firstFlight |
2000
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 1107C-Liberty
|
| gptkbp:is_used_in |
gptkb:Bell_Boeing_V-22_Osprey
|
| gptkbp:length |
1,200 mm
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notable_feature |
dual-fuel capability
|
| gptkbp:number_of_stages |
3
|
| gptkbp:operational_status |
military aviation
|
| gptkbp:powerOutput |
6,150 shp
|
| gptkbp:propulsion |
5.13
|
| gptkbp:service_ceiling |
25,000 ft
|
| gptkbp:type |
turbo-shaft engine
|
| gptkbp:weight |
1,200 kg
|