Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.18 m
|
| gptkbp:firstFlight |
1961
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
4.8 m
|
| gptkbp:manufacturer |
gptkb:Tumansky
|
| gptkbp:maximumSpeed |
9500 rpm
|
| gptkbp:notableFor |
high-speed performance
use in MiG-25 Foxbat |
| gptkbp:numberOfStages |
1
7 |
| gptkbp:thrust |
11200 kgf
7600 kgf |
| gptkbp:usedInAircraft |
gptkb:Mikoyan-Gurevich_MiG-25
Mikoyan-Gurevich MiG-25PU Mikoyan-Gurevich MiG-25RB Mikoyan-Gurevich MiG-25RU Mikoyan-Gurevich MiG-25U |
| gptkbp:weight |
1750 kg
|
| gptkbp:bfsParent |
gptkb:Mikoyan-Gurevich_MiG-25
gptkb:МиГ-25 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Tumansky R-15B-300
|