Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.89 m
|
| gptkbp:firstFlight |
1956
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
4.6 m
|
| gptkbp:manufacturer |
gptkb:Tumansky
|
| gptkbp:notableVariant |
R-11F-300
R-11F2S-300 |
| gptkbp:numberOfStages |
2
8 |
| gptkbp:status |
out of production
|
| gptkbp:successor |
gptkb:Tumansky_R-13
|
| gptkbp:thrust |
38.2 kN dry
56.4 kN with afterburner |
| gptkbp:type |
axial-flow turbojet
|
| gptkbp:usedInAircraft |
gptkb:Yakovlev_Yak-28
gptkb:Sukhoi_Su-15 gptkb:Mikoyan-Gurevich_MiG-21 |
| gptkbp:weight |
1,124 kg
|
| gptkbp:bfsParent |
gptkb:Yak-28
gptkb:WP-7B |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-11
|