Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
0.6
|
| gptkbp:category |
military aircraft engine
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
0.91 m
|
| gptkbp:firstFlight |
2008
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn AL-41F
|
| gptkbp:length |
4.9 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
|
| gptkbp:maximumSpeed |
15,000
|
| gptkbp:numberOfStages |
1 low-pressure, 1 high-pressure
4 low-pressure, 9 high-pressure |
| gptkbp:predecessor |
gptkb:Saturn_AL-31
|
| gptkbp:successor |
gptkb:Saturn_izdeliye_30
|
| gptkbp:thrust |
142 kN
88.3 kN |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:Sukhoi_Su-35
gptkb:Sukhoi_Su-57 |
| gptkbp:weight |
1600 kg
|
| gptkbp:bfsParent |
gptkb:Saturn_AL-31F
gptkb:Saturn_AL-41F1 |
| gptkbp:bfsLayer |
7
|