Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:trainer_aircraft
|
| gptkbp:combustionChambers |
annular
|
| gptkbp:compressionRatio |
two-stage low-pressure, five-stage high-pressure axial
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.57 m
|
| gptkbp:family |
gptkb:Ivchenko_AI-25
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:hasTower |
two-stage high-pressure, one-stage low-pressure
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ivchenko AI-25TLK turbofan
|
| gptkbp:length |
1.33 m
|
| gptkbp:manufacturer |
gptkb:Ivchenko-Progress
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
16.87 kN
|
| gptkbp:type |
low-bypass turbofan
|
| gptkbp:usedIn |
gptkb:Aero_L-39_Albatros
gptkb:Hongdu_JL-8 |
| gptkbp:weight |
330 kg
|
| gptkbp:bfsParent |
gptkb:Hongdu_JL-8
gptkb:Hongdu_K-8 |
| gptkbp:bfsLayer |
6
|