Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:regional_airliner
gptkb:trainer_aircraft |
| gptkbp:bypassRatio |
2.2:1
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.55 m
|
| gptkbp:firstFlight |
1966
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:length |
1.33 m
|
| gptkbp:manufacturer |
gptkb:Ivchenko-Progress
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Ivchenko_AI-25TL
|
| gptkbp:thrust |
14.7 kN
|
| gptkbp:usedInAircraft |
gptkb:Yakovlev_Yak-40
gptkb:Aero_L-39_Albatros gptkb:Hongdu_JL-8 |
| gptkbp:weight |
330 kg
|
| gptkbp:bfsParent |
gptkb:Yak-40
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Ivchenko AI-25 turbofan
|