GENERAL CHARACTERISTICS
Crew | Manned version: 2 (pilot & systems operator/observer) UAV version: 2 in ground station |
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Total length | 10.07 m | 33 ft |
Span | 12.69 m | 41 ft 7 in |
Cargo volume | 10.2 m3 | 360.21 cu ft |
Maximum takeoff weight | 2339 kg | 5,156 lb |
Regional air cargo service is a promising market: point-to-point air shuttles address the failure of road networks and the increase in the global flow of freight. In addition, the high and ever-increasing age of General Aviation aircraft worldwide suggests that a fleet renewal program will soon be initiated among aerial work operators, at the same time allowing them to switch to UAVs and green fuel.
For those reasons we have developed a robust twin hybrid-engine, stable manned and UAV aircraft which is laid out and certified for cargo operations and special missions. Thanks to very low turnaround times between flights this winged “estafette”, a french word for courier and also for a van, will contribute to upscaling General Aviation businesses by improving their efficiency and extending their range of services.
Local Freight & Mail
Passenger Transport
Suitable for remote areas
Main & regional hubs shuttle
Hybrid-engine UAV version
Scientific Surveys
Environment Management
Monitoring & Inspecting
Broadcasting
Skydiving
Surface Traffic Control
Flight Inspection & Calibration
Search & Rescue
Emergency & Disaster Relief
Air Ambulance /MEDEVAC
Maritime & Border Patrol
Light ISR /COMINT /SIGINT
Carrier Onboard Delivery
Light Logistics for Combat Zones
Airdropping of Paratroopers & Equipment
Crew | Manned version: 2 (pilot & systems operator/observer) UAV version: 2 in ground station |
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Total length | 10.07 m | 33 ft |
Span | 12.69 m | 41 ft 7 in |
Cargo volume | 10.2 m3 | 360.21 cu ft |
Maximum takeoff weight | 2339 kg | 5,156 lb |
Cruise speed | 284 km/h | 153 kt |
Range (payload in brackets) | 2028 km (500 kg) 1026 km (700 kg) | 1095 nmi (1,105 lb) 554 nmi (1,545 lb) |
Endurance (payload in brackets) | 9.5 hrs (500 kg) 5.6 hrs (700 kg) | 9.5 hrs (1,105 lb) 5.6 hrs (1,545 lb) |
Ceiling | 4572 m | 15,000 ft |
Takeoff run | 320 m | 1,050 ft |
Engine type | Hybrid electric/Jet A-1 fueled engines |
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