Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
axial flow
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Arkhip_Lyulka
|
| gptkbp:diameter |
1.09 m
|
| gptkbp:enteredService |
1970s
|
| gptkbp:firstFlight |
1965
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
AL-21 turbojet
|
| gptkbp:length |
4.77 m
|
| gptkbp:manufacturer |
gptkb:Lyulka
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
112 kN
|
| gptkbp:type |
afterburning turbojet
|
| gptkbp:usedInAircraft |
gptkb:Sukhoi_Su-22
gptkb:Mikoyan-Gurevich_MiG-23 gptkb:Sukhoi_Su-17 gptkb:Sukhoi_Su-24 Sukhoi Su-20 |
| gptkbp:weight |
1550 kg
|
| gptkbp:bfsParent |
gptkb:Lyulka_design_bureau
|
| gptkbp:bfsLayer |
7
|