Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
0.6
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
0.91 m
|
| gptkbp:features |
thrust vectoring nozzle
full authority digital engine control (FADEC) |
| gptkbp:firstFlight |
2010
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn AL-41F1 engine
|
| gptkbp:intendedUse |
fifth-generation fighter aircraft
|
| gptkbp:length |
4.99 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
gptkb:UMPO |
| gptkbp:numberOfStages |
1-stage high-pressure, 1-stage low-pressure
4-stage low-pressure, 9-stage high-pressure |
| gptkbp:predecessor |
gptkb:Saturn_AL-31
|
| gptkbp:status |
in production
|
| gptkbp:successor |
gptkb:Izdeliye_30
|
| gptkbp:thrust |
88.3 kN
147 kN |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Sukhoi_Su-57
gptkb:Sukhoi_Su-35S |
| gptkbp:weight |
1,600 kg
|
| gptkbp:bfsParent |
gptkb:Rostec
|
| gptkbp:bfsLayer |
5
|