Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
16:1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:engineType |
turbofan
propfan |
| gptkbp:firstFlight |
1991
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Kuznetsov NK-93
|
| gptkbp:intendedAircraft |
gptkb:aircraft
gptkb:Tupolev_Tu-204 gptkb:Ilyushin_Il-86 |
| gptkbp:intendedUse |
gptkb:aircraft
|
| gptkbp:length |
5.1 m
|
| gptkbp:mainRotorDiameter |
2900 mm
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:maximumSpeed |
180 kN
|
| gptkbp:notableFeature |
contra-rotating propfan
very high bypass ratio |
| gptkbp:numberOfAxles |
three
|
| gptkbp:status |
gptkb:prototype
|
| gptkbp:weapon |
8 front, 8 rear contra-rotating
|
| gptkbp:weight |
4100 kg
|
| gptkbp:bfsParent |
gptkb:Tupolev_Tu-330
|
| gptkbp:bfsLayer |
6
|