Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:basedOn |
gptkb:Saturn_AL-31F
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
0.905 m
|
| gptkbp:feature |
thrust vectoring nozzle
axial-flow afterburning low-bypass |
| gptkbp:firstFlight |
1990s
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn AL-31FP
|
| gptkbp:length |
4.99 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
|
| gptkbp:thrust |
12,500 kgf
7,800 kgf |
| gptkbp:usedInAircraft |
gptkb:Sukhoi_Su-35
gptkb:Sukhoi_Su-30MKI gptkb:Sukhoi_Su-30MKA gptkb:Sukhoi_Su-30MKM |
| gptkbp:weight |
1,520 kg
|
| gptkbp:bfsParent |
gptkb:Su-30MKM
gptkb:Sukhoi_Su-30MKA |
| gptkbp:bfsLayer |
7
|