Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.59
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:derivedFrom |
gptkb:AL-31F
|
| gptkbp:diameter |
0.905 m
|
| gptkbp:firstFlight |
1992
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
AL-31FN turbofan
|
| gptkbp:intendedUse |
Chinese fighter aircraft
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:Saturn
|
| gptkbp:numberOfStages |
1-stage high-pressure, 1-stage low-pressure
4-stage low-pressure, 9-stage high-pressure |
| gptkbp:operator |
gptkb:People's_Liberation_Army_Air_Force
|
| gptkbp:thrust |
yes
12,500 kgf (with afterburner) 7,800 kgf (dry) |
| gptkbp:usedInAircraft |
gptkb:Chengdu_J-10
gptkb:Shenyang_J-11 |
| gptkbp:weight |
1,520 kg
|
| gptkbp:bfsParent |
gptkb:J-10A
|
| gptkbp:bfsLayer |
7
|