Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:developedBy |
gptkb:Tumansky_R-11
|
| gptkbp:diameter |
1.02 m
|
| gptkbp:enteredService |
1967
|
| gptkbp:firstFlight |
1965
|
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-13
|
| gptkbp:length |
4.6 m
|
| gptkbp:manufacturer |
gptkb:Tumansky
|
| gptkbp:status |
out of production
|
| gptkbp:successor |
gptkb:Tumansky_R-25
|
| gptkbp:thrust |
40.2 kN
64.7 kN |
| gptkbp:type |
axial-flow turbojet
|
| gptkbp:usedInAircraft |
gptkb:Mikoyan-Gurevich_MiG-23
gptkb:Shenyang_J-8 gptkb:Mikoyan-Gurevich_MiG-21 |
| gptkbp:weight |
1125 kg
|
| gptkbp:bfsParent |
gptkb:Sergey_Tumansky
|
| gptkbp:bfsLayer |
6
|