Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Kamov_design_bureau
gptkb:Kamov_helicopters |
| gptkbp:aircraft_operated |
Ka-62
|
| gptkbp:armament |
gptkb:none
|
| gptkbp:capacity |
12 passengers
|
| gptkbp:crew |
2
|
| gptkbp:developer |
1990s to present
|
| gptkbp:diameter |
15.9 m
|
| gptkbp:engine |
T V3-117
|
| gptkbp:features |
coaxial rotor system
|
| gptkbp:first_flight |
gptkb:1998
|
| gptkbp:height |
4.5 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ka-60
|
| gptkbp:is_designed_to |
civil and military applications
|
| gptkbp:length |
15.9 m
|
| gptkbp:manufacturer |
gptkb:Kamov
|
| gptkbp:max_speed |
300 km/h
|
| gptkbp:notable_users |
gptkb:Russian_military
|
| gptkbp:origin |
gptkb:Russia
|
| gptkbp:produced_by |
in production
|
| gptkbp:range |
800 km
|
| gptkbp:role |
gptkb:public_transportation_system
|
| gptkbp:service_ceiling |
5000 m
|
| gptkbp:setting |
twin-engine
|
| gptkbp:type |
multi-role helicopter
|
| gptkbp:variant |
gptkb:Ka-60_Kasatka
|
| gptkbp:weight |
6000 kg
3800 kg |