Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.59:1
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:developedBy |
gptkb:Lyulka_design_bureau
|
| gptkbp:diameter |
1.28 m
|
| gptkbp:firstFlight |
1976
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Saturn_AL-41F
|
| gptkbp:thrust |
12,500 kgf (with afterburner)
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Chengdu_J-10
gptkb:Sukhoi_Su-27 gptkb:Sukhoi_Su-30 gptkb:Sukhoi_Su-35 gptkb:Sukhoi_Su-34 |
| gptkbp:weight |
1520 kg
|
| gptkbp:bfsParent |
gptkb:Sukhoi_Su-27
gptkb:Sukhoi_Su-30 |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn AL-31F
|