Statements (29)
| 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:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
1.905 m
|
| gptkbp:family |
gptkb:PS-90
|
| gptkbp:firstFlight |
1987
|
| gptkbp:fuelType |
Jet A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Aviadvigatel PS-90A
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:Aviadvigatel
|
| gptkbp:notableFeature |
modular design
FADEC control system first Russian engine to meet ICAO standards |
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfStages |
2 (high pressure), 4 (low pressure)
4 (low pressure), 10 (high pressure) |
| gptkbp:successor |
gptkb:PD-14
|
| gptkbp:thrust |
16000 kgf
|
| gptkbp:usedOn |
gptkb:Russian_Air_Force_aircraft
|
| gptkbp:weight |
3650 kg
|
| gptkbp:bfsParent |
gptkb:Tupolev_Tu-214
gptkb:Tupolev_Tu-204 gptkb:Ilyushin_Il-96-300 |
| gptkbp:bfsLayer |
6
|