Statements (54)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:armament |
none
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:crew |
2
|
| gptkbp:enginePower |
1,200 shp
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1980
|
| gptkbp:height |
4.57 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Westland 3800B
|
| gptkbp:length |
15.24 m
|
| gptkbp:manufacturer |
Westland_Aircraft
|
| gptkbp:maxSpeed |
250 km/h
|
| gptkbp:maxTakeoffWeight |
4,500 kg
|
| gptkbp:notableFeature |
fuel efficiency
high endurance modular design advanced communication systems advanced avionics advanced safety features low noise operation high reliability reliable performance high thrust-to-weight ratio easy maintenance low operational costs high stability customizable interiors high visibility cockpit crashworthy design large cabin space state-of-the-art navigation systems dual hydraulic systems retractable landing gear multi-role capability high payload capacity versatile mission capabilities excellent climb rate good maneuverability good visibility from cockpit versatile cargo options strong airframe robust landing gear high payload to weight ratio |
| gptkbp:passengerCapacity |
12
|
| gptkbp:primaryUser |
gptkb:British_Army
|
| gptkbp:productionYears |
1980-1990
|
| gptkbp:range |
800 km
|
| gptkbp:role |
utility helicopter
|
| gptkbp:rotorDiameter |
14.63 m
|
| gptkbp:services |
4,500 m
|
| gptkbp:successor |
gptkb:Westland_3900
|
| gptkbp:variant |
gptkb:Westland_3800B-1
Westland 3800B-2 |
| gptkbp:weight |
2,500 kg
|