Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
5.0:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:configuration |
two-spool
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.63 m
|
| gptkbp:family |
gptkb:IAE_V2500
|
| gptkbp:firstFlight |
1993
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| gptkbp:length |
2.3 m
|
| gptkbp:mainRotorDiameter |
1.63 m
|
| gptkbp:manufacturer |
gptkb:International_Aero_Engines
|
| gptkbp:marketedAs |
gptkb:International_Aero_Engines
|
| gptkbp:numberOfStages |
2
10 |
| gptkbp:thrust |
33,000 lbf
|
| gptkbp:usedOn |
gptkb:Airbus_A321
|
| gptkbp:weight |
2,260 kg
|
| gptkbp:bfsParent |
gptkb:A321-200
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
IAE V2533-A5
|