Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
two-spool axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.89 m
|
| gptkbp:enteredService |
1960s
|
| gptkbp:firstFlight |
1956
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
4.6 m
|
| gptkbp:manufacturer |
gptkb:Tumansky
|
| gptkbp:notableFor |
first Soviet two-spool engine
|
| gptkbp:numberOfStages |
2
6 |
| gptkbp:thrust |
3,800 kgf dry
5,600 kgf with afterburner |
| gptkbp:type |
afterburning turbojet
|
| gptkbp:usedInAircraft |
gptkb:Yakovlev_Yak-28
gptkb:Sukhoi_Su-15 gptkb:Mikoyan-Gurevich_MiG-21 |
| gptkbp:weight |
1,120 kg
|
| gptkbp:bfsParent |
gptkb:MiG-21F-13
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-11F-300
|