Statements (26)
Predicate | Object |
---|---|
gptkbp:instanceOf |
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
|
https://www.w3.org/2000/01/rdf-schema#label |
AL-31FN
|
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 gptkb:歼-10战斗机 |
gptkbp:bfsLayer |
6
|