Aviadvigatel PS-90A turbofan
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Ilyushin_Il-76
gptkb:Tupolev_Tu-214 gptkb:aircraft gptkb:Tupolev_Tu-204 |
| gptkbp:bypassRatio |
4.4:1
|
| gptkbp:certification |
1992
|
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
1.905 m
|
| gptkbp:family |
gptkb:PS-90
|
| gptkbp:firstFlight |
1987
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Aviadvigatel PS-90A turbofan
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:Aviadvigatel
|
| gptkbp:notableFeature |
first Russian high-bypass turbofan certified for civil use
|
| gptkbp:numberOfStages |
2 high-pressure, 4 low-pressure
4 low-pressure, 10 high-pressure |
| gptkbp:successor |
gptkb:PD-14
|
| gptkbp:thrust |
16000 kgf
|
| gptkbp:weight |
3650 kg
|
| gptkbp:bfsParent |
gptkb:Il-96-300
|
| gptkbp:bfsLayer |
5
|