Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
aerial refueling |
| gptkbp:bypassRatio |
2.4:1
|
| gptkbp:compressionRatio |
axial
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.18 m
|
| gptkbp:family |
gptkb:Soloviev_D-30
|
| gptkbp:firstFlight |
1979
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Soloviev D-30KP-2
|
| gptkbp:length |
3.98 m
|
| gptkbp:manufacturer |
gptkb:Soloviev_Design_Bureau
|
| gptkbp:numberOfAxles |
two
|
| gptkbp:thrust |
12,000 kgf
|
| gptkbp:turbineType |
axial
|
| gptkbp:usedInAircraft |
gptkb:Ilyushin_Il-76
gptkb:Beriev_A-50 gptkb:Ilyushin_Il-78 |
| gptkbp:weight |
2,350 kg
|
| gptkbp:bfsParent |
gptkb:Xian_Y-20
|
| gptkbp:bfsLayer |
6
|