Drone de mission à moyenne portée

SYSTÈME AÉRIEN DRONE à Moteur hybrid avec 8 hélices : injection électronique de carburant et réserve de batterie de 5 minutes de temps de vol.

1 hEUrE
AVEC 12lb (5.5 kg)
CapacitÉ DE CHARGE

100 km / 60 miles*

DISTANCE DE CONTRÔLE Video

5+ Heures

NON PAYLOAD MAX Flight Endurance

< 5 minutes

TEMPS D'INSTALLATION

LA RESERVE DE BATTERIE assurer la sécurité des charges utiles de grande valeur.

Le multirotor hybride le plus facile, le plus sûr et le plus endurant sur le marché

SPéCIFICATIONS

Maximum Speed	36 mph (57 km/hr)
Cruise Ground Speed	22 mph (35 km/hr)
Maximum Endurance *	5+ hours without payload 2.5+ hours with 6.5 lb. (3 kg) payload 1+ hour with 11 lb. (5 kg) payload
Maximum Expected Range (at cruise speed)	No Payload – 110 miles (177 km)
Maximum Tested Wind Speeds	25 mph (35 km/hr)
Maximum Payload Capacity	12 lb.+ (5.5 kg) payload with 2.2 lb (1 kg) fuel (1 hour).
Minimum Expected Temperature	15°F (-10°C)
Maximum Expected Temperature	122°F (50°C)
Size
Tip-to-Tip length	Arms removed: 2 feet x 2.66 feet (0.6 m x 0.81 m) Ready to fly: 6.5 feet x 6.25 feet (2 m x 1.9 m)
Minimum Height	14.5” (0.37 m)
Height	Customizable to fit payload
Maximum Takeoff Weight	42 lb (19 kg)
Controls and Communication
Radio Frequency	Configurable. Contact us.
Maximum Expected Telemetry Distance	6.2 miles (10 km)
Flight Modes	Manual through remote controller – Stabilize – Altitude (barometer- and GPS-based) – Position (GPS-based) GPS-based waypoint autonomy – Survey – Waypoint navigation and payload control Automatic land and takeoff
Radio Telemetry Link Encryption	AES128 by default. Up to AES256.
Electronics, software and firmware
Autopilot Firmware	Janus Autopilot™. Proprietary. PX4-based.
Engine Control Firmware and Electronics	Proprietary.
Autopilot Electronics	Proprietary. Pixhawk-based. Hardened and protected
Ground Control Station
Ground Control Software	Janus Ground Control Station™ (jGCS). Proprietary. QGroundControl-based with engine telemetry and control.
Power System
System	Windows 10 Laptop
Fuel Delivery	G2K proprietary hybrid gasoline-electric propulsion system
Ground Control Hardware	Electronic Fuel Injection
Electrical Conversion Efficiency	> 95%
Battery Flight Time	5 minutes maximum at 42 lb (19 kg) takeoff weight. (can increase by request)
Battery Type	Lithium Polymer
Gasoline/Petrol Type	91 Octane or above

* Flight times were measured at MSL 0’ in 50-75°F temperatures. Actual flight times depend on temperature, altitude,
wind and other environmental conditions.

** Tested operating conditions. Actual range may be greater.

Specifications are subject to change without notice.

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