Jupiter-H2. Specifications. A photo.

Jupiter-H2 is a multi-functional unmanned aerial vehicle developed by the British company UK Smart Energy.

The unmanned aircraft of the Jupiter-H2 model was designed for civilian applications, and the device has enough broad functionality, which means that this drone can perform a wide range of various tasks, among which aerial photography and aerial photography, observation, patrol and monitoring missions. The key feature of this UAV is the fact that the device is powered by hydrogen fuel cells, which not only ensures environmental compatibility while flying, but also allows the drone to remain in the air for a fairly long period of time.

The British multi-purpose unmanned aerial vehicle model Jupiter-H2 was designed in a quadrocopter configuration, which allows the drone to be operated in almost any terrain conditions, taking off and landing in a vertical plane. If necessary, the device may hang during the flight over objects or the terrain for a more thorough study of them. Compact dimensions of the UAV Jupiter-H2 provide ease of operation and transportation.

The power section of the civil multifunctional unmanned aerial vehicle Jupiter-H2 is represented by four electric motors that are capable of accelerating the air to the maximum flight speed of 45 km / h, with autonomy of being in flight up to two hours.

Technical specifications of Jupiter-H2.

• Length: Unknown;
• Width: unknown;
• Height: Unknown;
• Maximum takeoff weight: unknown;
• Cruising flight speed: 20 km \ h .;
• Maximum flight speed: 45 km \ h .;
• Maximum flight distance: 5 km .;
• Maximum flight height: 1200 m .;
• aircraft engine type: Electric;
• Powerplant: unknown;
• Power: unknown.

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