Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:trainer_aircraft
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.57 m
|
| gptkbp:firstFlight |
1966
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ivchenko AI-25TL
|
| gptkbp:length |
1.33 m
|
| gptkbp:manufacturer |
gptkb:Ivchenko-Progress
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfStages |
2
2 (axial) + 1 (centrifugal) |
| gptkbp:successor |
gptkb:Ivchenko_AI-25TLK
|
| gptkbp:thrust |
16.9 kN
|
| gptkbp:type |
low-bypass turbofan
|
| gptkbp:usedInAircraft |
gptkb:Aero_L-39_Albatros
gptkb:Hongdu_JL-8 gptkb:Aero_L-59 |
| gptkbp:weight |
330 kg
|
| gptkbp:bfsParent |
gptkb:Aero_L-39_Albatros
gptkb:L-39 gptkb:L-39_Albatros |
| gptkbp:bfsLayer |
6
|