Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.02 m
|
| gptkbp:firstFlight |
1965
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-13-300
|
| gptkbp:length |
4.6 m
|
| gptkbp:manufacturer |
gptkb:Tumansky
|
| gptkbp:notableFeature |
improved high-altitude performance
|
| gptkbp:numberOfStages |
2
8 |
| gptkbp:predecessor |
gptkb:Tumansky_R-11
|
| gptkbp:successor |
gptkb:Tumansky_R-25
|
| gptkbp:thrust |
40.2 kN
|
| gptkbp:thrustAfterburner |
64.7 kN
|
| gptkbp:type |
afterburning turbojet
|
| gptkbp:usedInAircraft |
gptkb:Shenyang_J-8
gptkb:Sukhoi_Su-15 gptkb:Mikoyan-Gurevich_MiG-21 |
| gptkbp:weight |
1125 kg
|
| gptkbp:bfsParent |
gptkb:MiG-21MF
gptkb:2_×_Tumansky_R-13-300_turbojets |
| gptkbp:bfsLayer |
7
|