Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
8.5:1
|
| gptkbp:certification |
gptkb:Russian_Federal_Air_Transport_Agency
2018 |
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:developedBy |
gptkb:United_Engine_Corporation
|
| gptkbp:diameter |
1.9 m
|
| gptkbp:family |
gptkb:PD-14_engine_family
|
| gptkbp:firstFlight |
2015
|
| gptkbp:firstRun |
2012
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:hasConcept |
two-spool
|
| gptkbp:intendedAircraft |
gptkb:Irkut_MC-21
|
| gptkbp:length |
4.9 m
|
| gptkbp:mainRotorDiameter |
1.9 m
|
| gptkbp:manufacturer |
gptkb:Aviadvigatel
|
| gptkbp:marketedAs |
narrow-body airliners
|
| gptkbp:notableFeature |
first all-new Russian commercial turbofan since Soviet era
|
| gptkbp:numberOfStages |
8
|
| gptkbp:status |
in production
|
| gptkbp:successor |
gptkb:PS-90A
|
| gptkbp:thrust |
14000 kgf
|
| gptkbp:usedOn |
gptkb:Irkut_MC-21
|
| gptkbp:bfsParent |
gptkb:Irkut_MC-21
gptkb:Yakovlev_MC-21 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Aviadvigatel PD-14
|