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CANADA |
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Prime Manu.
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UAV Designation
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Production status
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Power plants
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Dimensions (m)
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Wieghts (kg)
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Production
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Operation
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Purpose
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Mission payload
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Launch, take-off type
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Recovery, landing type
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Min ground crews need
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System composite
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Datalink, comm frequency
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Engine
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Propulsion
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Wing span
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Wing area (§³)
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Length overall
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Height overall
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Wheel track
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Wheel base
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Wing aspect ratio
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Fuselage max width
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Weight empty
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Max fuel weight
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Max Payload
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Max T-O/launch weight
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Max level speed (kt)
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Cruising speed (kt)
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Loiter speed (kt)
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Stall speed (kt)
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Service Ceiling (ft)
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Max rate of climb (ft/min)
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Range (nm)
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Max Endurance (h)
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Bombardier
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CL-89
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Complete | Complete | Deployed | Division-level recoverable surveillance drone | Day photo camera (Zeiss KRb 8/24C). Night Vinten Type 201 IRLS. | Booster rocket | Parachute / airbag | I/J-band transponder | One 125 lb st Williams WR2-6 turbojet. | 0.94 |
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3.73 | Di 0.33 | 78.2 | 17-20 | 108 | 400 | 10,000 | 32 / 38 (with extended range fuel tank) | 0.2 | ||||||||||||||
| Teamed with Germany, UK in 1965 and shared 282 dornes. | 20 systems, 40 launchers, more than 500 drones for Canada, Germany, UK, Italy and France. | 
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CL-289
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Complete | Complete | Deployed | Turbojet | 4.3 |
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75 | 650 | 3,900 | 108 | 0.5 | Teamed with Dornier | |||||||||||||||||||||||
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CL-227 Sentinel (Army) |
Complete |
Complete |
Deployed |
Land-base VTOL multi-application |
FLIR, Day TV, comm relay, electronic jammer, decoys, snobuoy dispensers, mine detector, ECM, radars and laser designators |
Conventional VTO |
Sierra Nevada UCARS system. |
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GCS, MCPS |
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One 51.5 shp Williams WTS34-16 turboshaft (- Pase3) Now one 60 shp Williams WTS125 heavy-fuel turboshaft. |
Rotor |
Rotor Dia 2.80 |
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Body Dia 0.64 |
1.64 |
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111 |
Multi fuel diesel, JP-5, Jet-A, heavy fuel. 54 kg |
45 |
227 |
77 |
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9,840 |
900 |
32.4 |
3.5 |
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First flight on 25 August 1978. |
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US Army, US Navy(1993), |
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Prime Manu.
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UAV Designation
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Production status
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Operational status
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Power plants
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Dimensions (m)
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Wieghts (kg)
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Performance
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Comments
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Development
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Production
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Operation
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Purpose
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Mission payload
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Launch, take-off type
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Recovery, landing type
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Min ground crews need
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System composite
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Datalink, comm frequency
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Engine
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Propulsion
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Wing span
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Wing area (§³)
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Length overall
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Height overall
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Wheel track
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Wheel base
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Wing aspect ratio
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Fuselage max width
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Weight empty
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Max fuel weight
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Max Payload
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Max T-O/launch weight
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Max level speed (kt)
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Cruising speed (kt)
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Loiter speed (kt)
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Stall speed (kt)
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Service Ceiling (ft)
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Max rate of climb (ft/min)
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Range (nm)
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Max Endurance (h)
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| Bombardier |
CL-227 Sea Sentinel (Navy, Marine) |
Complete |
Complete |
Deployed |
Configured for shipborne applications |
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US Marine (MAVUS) |
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CL-227 Puma (TUAV) |
Comple.te |
Complete |
Deployed |
Modified version for TUAV competition |
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First flight in March 1996 |
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CL-327 Guardian
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Complete | Underway | Deployed | Multi-role VTOL surveillance |
EO/IR, comm relay, SAR, active ECM. |
Conventional VTO |
Sierra Nevada UCARS system. |
2 for setup and operate. | downsized GCS, TCS | G/H-band | One 125 shp Williams WTS117-5 heavy-fuel turboshaft. | Rotor | Rotor dia 4.0 |
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0.76 | 1.84 | 150 | 150 kg | 110 | 235 kg (std) 350 kg (max) | 85 | 75 | 50 | 18,000 | 1,500 | 54 | 6.2 | No Tail; Counter-Rotating Rotors | |||||||
| First flight on 30 November, 1997. | 
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CL-427 (TUAV)
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Complete | Underway | // | // |
Conventional VTO |
Sierra Nevada UCARS system. | // | // | // | One 125 shp Williams WTS117-5 heavy-fuel turboshaft. | Rotor = 13 |
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2.12 | 135 | 160 kg | 150 | 300 kg (std) 340 kg (max) | 120 | 18,000 | 1,400 | 108 | 8.0 | No Tail; Counter-Rotating Rotors | ||||||||||||
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Prime Manu.
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UAV Designation
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Production status
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Operational status
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Power plants
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Dimensions (m)
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Wieghts (kg)
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Performance
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Comments
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Development
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Production
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Operation
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Purpose
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Mission payload
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Launch, take-off type
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Recovery, landing type
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Min ground crews need
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System composite
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Datalink, comm frequency
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Engine
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Propulsion
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Wing span
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Wing area (§³)
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Length overall
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Height overall
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Wheel track
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Wheel base
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Wing aspect ratio
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Fuselage max width
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Weight empty
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Max fuel weight
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Max Payload
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Max T-O/launch weight
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Max level speed (kt)
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Cruising speed (kt)
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Loiter speed (kt)
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Stall speed (kt)
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Service Ceiling (ft)
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Max rate of climb (ft/min)
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Range (nm)
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Max Endurance (h)
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Pan Atlantic |
LEAP |
Underway |
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Remotely piloted airship |
Camera or others as required. |
Conventional airship launch. |
Cenventional airship landing. |
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Three piston engines. |
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20.42 |
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3.35 |
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32.6 |
119.5 |
26 |
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1.1 |
4 - 6 |
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