Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:configuration |
axial flow
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:diameter |
0.905 m
|
| gptkbp:exportedTo |
gptkb:China
|
| gptkbp:family |
gptkb:AL-31
|
| gptkbp:firstFlight |
1990s
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:intendedUse |
export to China
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
|
| gptkbp:numberOfAxles |
two
|
| 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 |
12,500 kgf (with afterburner)
7,800 kgf (dry) |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Chengdu_J-20_(early_prototypes)
gptkb:Chengdu_J-10 |
| gptkbp:weight |
1,520 kg
|
| gptkbp:bfsParent |
gptkb:J-10B
gptkb:J-10_multirole_fighter |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
AL-31FN
|