Statements (29)
| 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:firstFlight |
1966
|
| https://www.w3.org/2000/01/rdf-schema#label |
Soloviev D-30
|
| gptkbp:length |
3.98 m
|
| gptkbp:manufacturer |
gptkb:Soloviev_Design_Bureau
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Aviadvigatel_PS-90
|
| gptkbp:thrust |
6,800 kgf
|
| gptkbp:type |
two-shaft turbofan
|
| gptkbp:usedInAircraft |
gptkb:Ilyushin_Il-76
gptkb:Tupolev_Tu-134 gptkb:Tupolev_Tu-154M gptkb:Beriev_A-50 gptkb:Ilyushin_Il-62M gptkb:Tupolev_Tu-144D |
| gptkbp:variant |
gptkb:D-30F6
gptkb:D-30KP gptkb:D-30KU gptkb:D-30KU-154 |
| gptkbp:weight |
1,550 kg
|
| gptkbp:bfsParent |
gptkb:Ilyushin_Il-62
gptkb:Tupolev_Tu-134 gptkb:Tu-134 |
| gptkbp:bfsLayer |
6
|