Statements (59)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft
|
| gptkbp:armament |
none
|
| gptkbp:crew |
2
|
| gptkbp:enginePower |
1000 hp
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1990
|
| gptkbp:height |
3.5 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
KA-36
|
| gptkbp:length |
12.5 m
|
| gptkbp:manufacturer |
gptkb:Kazan_Helicopter_Plant
|
| gptkbp:maxSpeed |
250 km/h
|
| gptkbp:maxTakeoffWeight |
4000 kg
|
| gptkbp:notableFeature |
high endurance
modular design advanced avionics high reliability high maneuverability low noise levels advanced navigation systems quick response time high operational flexibility user-friendly controls large cabin space advanced flight control system modern safety features multi-role capability high payload capacity versatile mission capabilities good fuel efficiency environmental adaptability high situational awareness short takeoff and landing capability advanced autopilot system folding rotor blades suitable for various missions easy access to components good stability in flight low maintenance cost good handling characteristics good visibility from cockpit reliable communication systems effective thermal insulation good performance in adverse weather conditions integrated flight management system effective cargo handling capabilities quick maintenance turnaround high_altitude_performance |
| gptkbp:passengerCapacity |
6
|
| gptkbp:primaryUser |
gptkb:Russian_military
|
| gptkbp:productionStartYear |
1990
|
| gptkbp:productionYears |
present
|
| gptkbp:range |
600 km
|
| gptkbp:role |
utility helicopter
|
| gptkbp:rotorDiameter |
12 m
|
| gptkbp:services |
5000 m
|
| gptkbp:variant |
KA-36A
KA-36B KA-36C |
| gptkbp:weight |
2500 kg
|