Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
civil aviation |
| gptkbp:bypassRatio |
2.4:1
|
| gptkbp:category |
medium-bypass turbofan
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.22 m
|
| gptkbp:firstFlight |
1966
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:length |
4.84 m
|
| gptkbp:manufacturer |
gptkb:Soloviev_Design_Bureau
|
| gptkbp:notableVariant |
gptkb:D-30F6
gptkb:D-30KP gptkb:D-30KU gptkb:D-30KU-154 |
| gptkbp:numberOfAxles |
two
|
| gptkbp:numberOfStages |
three low-pressure, ten high-pressure
two low-pressure, four high-pressure |
| gptkbp:status |
in service
|
| gptkbp:thrust |
6,800–12,000 kgf
|
| gptkbp:usedInAircraft |
gptkb:Ilyushin_Il-62
gptkb:Ilyushin_Il-76 gptkb:Tupolev_Tu-134 gptkb:Tupolev_Tu-154M |
| gptkbp:weight |
2,350 kg
|
| gptkbp:bfsParent |
gptkb:Perm_Engine_Design_Bureau
gptkb:NPO_Saturn gptkb:Aviadvigatel |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
D-30 engine
|