Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
0.6:1
|
| gptkbp:controls |
full authority digital engine control (FADEC)
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
0.91 m
|
| gptkbp:firstFlight |
2010
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn AL-41F1
|
| gptkbp:length |
4.9 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
gptkb:UMPO |
| gptkbp:numberOfStages |
4-stage low-pressure, 9-stage high-pressure
1-stage high-pressure, 2-stage low-pressure |
| gptkbp:relatedTo |
gptkb:Saturn_AL-41F
gptkb:Saturn_AL-31 |
| gptkbp:thrust |
147 kN
93 kN |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Sukhoi_Su-57
Sukhoi Su-35 (prototype) |
| gptkbp:weight |
1,600 kg
|
| gptkbp:bfsParent |
gptkb:Su-57
|
| gptkbp:bfsLayer |
6
|