Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
4.4:1
|
| gptkbp:certification |
1992
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
1.9 m
|
| gptkbp:family |
PS-90 family
|
| gptkbp:firstFlight |
1987
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Aviadvigatel PS-90
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:Aviadvigatel
|
| gptkbp:notableFeature |
modular design
FADEC control system first Russian engine to meet ICAO Stage 3 noise requirements |
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfSpools |
2
|
| gptkbp:predecessor |
gptkb:Soloviev_D-30
|
| gptkbp:successor |
gptkb:PD-14
|
| gptkbp:thrust |
16000 kgf
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:usedInAircraft |
gptkb:Ilyushin_Il-76
gptkb:Tupolev_Tu-214 gptkb:aircraft gptkb:Tupolev_Tu-204 Berkut VL |
| gptkbp:variant |
gptkb:PS-90A
PS-90A2 PS-90A-42 PS-90A-76 PS-90A3 |
| gptkbp:weight |
2950 kg
|
| gptkbp:bfsParent |
gptkb:Soloviev_D-30
|
| gptkbp:bfsLayer |
7
|