Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:trainer_aircraft
|
| gptkbp:compressionRatio |
axial
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.75 m
|
| gptkbp:family |
gptkb:Ivchenko_AI-25
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
1.55 m
|
| gptkbp:manufacturer |
gptkb:Ivchenko-Progress
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfStages |
2
5 |
| gptkbp:status |
in service
|
| gptkbp:thrust |
16.9 kN
|
| gptkbp:type |
low-bypass turbofan
|
| gptkbp:usedInAircraft |
gptkb:Aero_L-39_Albatros
gptkb:Hongdu_JL-8 |
| gptkbp:weight |
330 kg
|
| gptkbp:bfsParent |
gptkb:Ivchenko_AI-25TL
gptkb:K-8_Karakorum |
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Ivchenko AI-25TLK
|