CL-327 Specifications | |
Country of Origin | Canada |
Builder | |
Missions |
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Engine | 1 Williams International WTS-125 turboshaft 125 shp flat rated at 100 shp |
Height | 6 ft 0 in 1.84 m |
Rotor diameter | 13 ft 1 in 4.00 m |
Gross takeoff mass | 770 lbs. 350 kg |
Empty weight | (no payload, no fuel) 330 lbs. 150 kg |
Payload carrying capacity | 220 lbs. 100 kg |
Maximum endurance | 6.25 hours |
Time on station at 100 km | 4.75 hours |
Maximum speed | 157 km/h / 85 kts |
Climb rate | 7.6 m/sec / 1,500 ft/min |
Ceiling | 5,500 m / 18,000 ft |
Sensor |
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Datalink |
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Guidance and navigation |
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Image Exploitation |
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Crew | |
Cost | |
User Countries |
Air Views Ground View Bottom Shots Preparation for Launch Inside Views Communication |