Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
0.74
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
0.92 m
|
| gptkbp:features |
thrust vectoring nozzle
full authority digital engine control (FADEC) |
| gptkbp:firstFlight |
2008
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:generation |
4++ generation engine
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn AL-41F1S
|
| gptkbp:length |
4.99 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
|
| gptkbp:relatedTo |
gptkb:Saturn_AL-41F1
gptkb:Saturn_AL-31 |
| gptkbp:thrust |
142 kN
86.3 kN |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Sukhoi_Su-35
gptkb:Sukhoi_Su-57 |
| gptkbp:weight |
1,600 kg
|
| gptkbp:bfsParent |
gptkb:Su-35
|
| gptkbp:bfsLayer |
6
|