Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
axial flow
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.89 m
|
| gptkbp:firstFlight |
1956
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-27-300
|
| gptkbp:length |
3.8 m
|
| gptkbp:manufacturer |
gptkb:Tumansky
|
| gptkbp:numberOfStages |
1
7 |
| gptkbp:status |
out of production
|
| gptkbp:thrust |
5,700 lbf
|
| gptkbp:thrustAfterburner |
7,165 lbf
|
| gptkbp:type |
afterburning turbojet
|
| gptkbp:usedInAircraft |
gptkb:Mikoyan-Gurevich_MiG-19
|
| gptkbp:weight |
900 kg
|
| gptkbp:bfsParent |
gptkb:Yakovlev_Yak-36
|
| gptkbp:bfsLayer |
8
|