Statements (22)
Predicate | Object |
---|---|
gptkbp:instanceOf |
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
|
https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-11F-300
|
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
|