Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
0.59
|
| gptkbp:combustors |
annular
|
| gptkbp:compressionRatio |
4-stage low-pressure, 9-stage high-pressure axial
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.28 m
|
| gptkbp:firstFlight |
1976
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:hasTower |
single-stage high-pressure, single-stage low-pressure
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn AL-31
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
|
| gptkbp:notableVariant |
gptkb:AL-31F
gptkb:AL-31FN AL-31FP AL-31FM |
| gptkbp:status |
in service
|
| gptkbp:successor |
Saturn AL-41
|
| gptkbp:thrust |
76.2 kN
|
| gptkbp:thrustAfterburner |
122.6 kN
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Shenyang_J-11
gptkb:Shenyang_J-16 gptkb:Sukhoi_Su-27 gptkb:Sukhoi_Su-30 gptkb:Sukhoi_Su-35 gptkb:Sukhoi_Su-34 |
| gptkbp:weight |
1520 kg
|
| gptkbp:bfsParent |
gptkb:Saturn_AL-41F1_engine
|
| gptkbp:bfsLayer |
6
|