Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
4.4:1
|
| gptkbp:certification |
1992
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
1.905 m
|
| gptkbp:family |
gptkb:PS-90
|
| gptkbp:firstFlight |
1992
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:intendedUse |
long-range widebody aircraft
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:Aviadvigatel
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfStages |
2 high-pressure, 4 low-pressure
4 low-pressure, 10 high-pressure |
| gptkbp:thrust |
16,000 kgf
|
| gptkbp:usedInAircraft |
gptkb:Ilyushin_Il-96-300
Ilyushin Il-96-400 Ilyushin Il-96T |
| gptkbp:weight |
3,650 kg
|
| gptkbp:bfsParent |
gptkb:Ил-96-400М
gptkb:Il-96-400 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Aviadvigatel PS-90A1
|