Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:crew |
5
|
| gptkbp:engine |
gptkb:Soloviev_D-25V
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1957
|
| gptkbp:firstFlownBy |
Rafail Kaprelian
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mil Mi-6 (early prototypes)
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:role |
heavy transport helicopter
|
| gptkbp:rotorConfiguration |
single main rotor with tail rotor
|
| gptkbp:status |
gptkb:prototype
|
| gptkbp:successor |
Mil Mi-6 (production version)
|
| gptkbp:bfsParent |
gptkb:Shvetsov_ASh-82V_radial_engine
|
| gptkbp:bfsLayer |
7
|