Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
11,000 kg
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:crew |
5
|
| gptkbp:developedBy |
gptkb:Mil_Mi-10
|
| gptkbp:emptyWeight |
17,500 kg
|
| gptkbp:engine |
gptkb:Soloviev_D-25V
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1965
|
| gptkbp:height |
7.80 m
|
| gptkbp:length |
32.86 m
|
| gptkbp:mainRotorDiameter |
35.00 m
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:maximumSpeed |
220 km/h
|
| gptkbp:maxTakeoffWeight |
38,000 kg
|
| gptkbp:notableFeature |
shorter landing gear
ventral gondola for load operations |
| gptkbp:numberOfEngines |
2
|
| gptkbp:powerplant |
4,100 kW each
|
| gptkbp:range |
250 km
|
| gptkbp:role |
flying crane
|
| gptkbp:serviceCeiling |
3,000 m
|
| gptkbp:status |
retired
|
| gptkbp:usedBy |
gptkb:Aeroflot
gptkb:Soviet_Air_Force |
| gptkbp:bfsParent |
gptkb:2_×_Soloviev_D-25V_turboshaft
gptkb:Soloviev_D-25V |
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Mil Mi-10K
|