Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Arkhip_Lyulka
|
| gptkbp:diameter |
1.09 m
|
| gptkbp:firstFlight |
1952
|
| gptkbp:length |
5.3 m
|
| gptkbp:manufacturer |
gptkb:Lyulka
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Lyulka_AL-21
|
| gptkbp:thrust |
9,600 kgf
6,240 kgf (dry) |
| gptkbp:type |
axial-flow turbojet
|
| gptkbp:usedInAircraft |
gptkb:Tupolev_Tu-128
gptkb:Sukhoi_Su-17 gptkb:Sukhoi_Su-7 gptkb:Sukhoi_Su-9 |
| gptkbp:weight |
1,350 kg
|
| gptkbp:bfsParent |
gptkb:Lyulka_design_bureau
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
AL-7 turbojet
|