Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:armament |
gptkb:30_mm_2A42_cannon
rockets air-to-air missiles anti-tank guided missiles |
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
1
|
| gptkbp:developedBy |
gptkb:Kamov_V-80
|
| gptkbp:ejectionSeat |
yes
|
| gptkbp:emptyWeight |
7,700 kg
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1982
|
| gptkbp:height |
4.93 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ka-50 helicopter
|
| gptkbp:introduced |
1995
|
| gptkbp:length |
16.0 m
|
| gptkbp:manufacturer |
gptkb:Kamov
|
| gptkbp:maximumSpeed |
310 km/h
|
| gptkbp:maxTakeoffWeight |
10,800 kg
|
| gptkbp:NATOReportingName |
gptkb:Hokum_A
|
| gptkbp:nickname |
gptkb:Black_Shark
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:primaryUser |
gptkb:Russian_Air_Force
|
| gptkbp:range |
545 km
|
| gptkbp:relatedTo |
gptkb:Ka-52
|
| gptkbp:rotorConfiguration |
coaxial rotors
|
| gptkbp:usedInConflict |
gptkb:Second_Chechen_War
|
| gptkbp:bfsParent |
gptkb:Ka-52_helicopter
|
| gptkbp:bfsLayer |
6
|