Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
civil aviation |
| gptkbp:bypassRatio |
2.4:1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.22 m
|
| gptkbp:family |
gptkb:Soloviev_D-30
|
| gptkbp:firstFlight |
1971
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
D-30KU
|
| gptkbp:length |
4.84 m
|
| gptkbp:manufacturer |
gptkb:Aviadvigatel
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfStages |
2 (low pressure), 2 (high pressure)
3 (low pressure), 10 (high pressure) |
| gptkbp:successor |
gptkb:D-30KP
|
| gptkbp:thrust |
12,000 kgf
|
| gptkbp:usedInAircraft |
gptkb:Ilyushin_Il-76
gptkb:Ilyushin_Il-62M |
| gptkbp:weight |
2,350 kg
|
| gptkbp:bfsParent |
gptkb:Soloviev_D-30
|
| gptkbp:bfsLayer |
7
|