Statements (56)
Predicate | Object |
---|---|
gptkbp:instanceOf |
gptkb:helicopter
|
gptkbp:armament |
none
|
gptkbp:crew |
2
|
gptkbp:engineType |
turbine engine
|
gptkbp:firstFlight |
1971
|
gptkbp:height |
3.5 meters
|
https://www.w3.org/2000/01/rdf-schema#label |
Westland 109S Mk VII
|
gptkbp:length |
12.8 meters
|
gptkbp:manufacturer |
Westland_Aircraft
|
gptkbp:maxSpeed |
130 knots
|
gptkbp:maxTakeoffWeight |
3,600 kg
|
gptkbp:notableFeature |
enhanced situational awareness
fuel efficiency high endurance modular design safety features advanced communication systems advanced avionics low noise operation high reliability high maneuverability low maintenance costs advanced safety systems advanced navigation systems customizable configurations easy maintenance weather-resistant design high operational flexibility retractable landing gear multi-role capability high payload capacity versatile mission capabilities dual control system integrated flight control systems quick deployment capabilities good visibility from cockpit strong airframe high performance in adverse conditions user-friendly cockpit layout effective load distribution high_altitude_performance |
gptkbp:passengerCapacity |
6
|
gptkbp:productionYears |
1971-1985
|
gptkbp:range |
600 nautical miles
|
gptkbp:role |
utility helicopter
|
gptkbp:rotorDiameter |
11.0 meters
|
gptkbp:services |
15,000 feet
|
gptkbp:successor |
gptkb:Westland_114
|
gptkbp:usedBy |
gptkb:United_Kingdom
|
gptkbp:variant |
gptkb:Westland_109S_Mk_II
gptkb:Westland_109S_Mk_VI gptkb:Westland_109S_Mk_III gptkb:Westland_109S_Mk_IV gptkb:Westland_109S_Mk_V Westland_109S_Mk_I |
gptkbp:weight |
2,500 kg
|