Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.57
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.46 m
|
| gptkbp:firstFlight |
1975
|
| https://www.w3.org/2000/01/rdf-schema#label |
D-30F6
|
| gptkbp:length |
6.48 m
|
| gptkbp:manufacturer |
gptkb:Soloviev_Design_Bureau
|
| gptkbp:maximumThrustDry |
93.1 kN
|
| gptkbp:maximumThrustWithAfterburner |
152 kN
|
| gptkbp:numberOfAxles |
3
|
| gptkbp:numberOfStages |
2 high-pressure, 2 low-pressure
3 low-pressure, 10 high-pressure |
| gptkbp:relatedTo |
gptkb:Soloviev_D-30
|
| gptkbp:thrust |
152 kN
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:Mikoyan_MiG-31
|
| gptkbp:weight |
2416 kg
|
| gptkbp:bfsParent |
gptkb:Soloviev_D-30
|
| gptkbp:bfsLayer |
7
|