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At a glance
Measured figures
Length
Single source6.2 m (20 ft 4 in)[source]
Evo II Pro V3 · folded
Single sourceConfiguration
| Specification | Airbus Helicopters VSR700 | Autel Evo |
|---|---|---|
| Type | unmanned reconnaissance helicopter[source] | Unmanned aerial vehicle[source] |
| National origin | France[source] | China[source] |
| Manufacturer | Airbus Helicopters[source] | Autel Robotics[source] |
| First flight | 8 November 2019[source] | — |
Evo II Pro V3 · Length
Single source0.457 m (1 ft 6 in) (0.230 m (9.1 in) folded)[source]
Main rotor diameter
Single source7.2 m (23 ft 7 in)[source]
Evo II Pro V3 · Range
Single source25 km (16 mi, 13 nmi)[source]
1 × Thielert Centurion 2.0 diesel engine
Single source1 × Thielert Centurion 2.0 diesel engine, 116 kW (155 hp)[source]
100nm (185 km, 115 miles) from the boat
Single sourceEndurance
Single sourceor >
Single source10 hours or >8 hours 100nm (185 km, 115 miles) from the boat.[source]
Endurance: 10 hours[source]Airbus Helicopters VSR700 · Specifications · Endurance: 10 hours or >8 hours 100nm (185 km, 115 miles) from the boat.
Evo II Pro V3 · Endurance
Single source39 minutes[source]
Evo II Pro V3 · 1,600 ft/min
Single source8 m/s (1,600 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Developed from | Guimbal Cabri G2[source] | — |
|---|
| Capacity | 100 kg (220 lb) mission payload[source] | — |
|---|
| Fuel capacity | 185 L (41 imp gal; 49 US gal)[source] | — |
|---|
| Role | unmanned reconnaissance helicopter being[source] | — |
|---|
| Source measurement | Developed by Airbus, the VSR700 is based on the Cabri G2 light helicopter, developed and produced by Hélicoptères Guimbal . Airbus was awarded a contract by the French Navy toward the end of 2017. With a maximum take-off weight around 700 kg (1,500 lb), it is a larger aircraft than the Austrian Camcopter S-100 which the French Navy has been operating since 2012.[source]Airbus Helicopters VSR700 · Design and development; only the objects and conditions stated in this passage Capacity: 100 kg (220 lb) mission payload[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage Length: 6.2 m (20 ft 4 in)[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage Width: 1.24 m (4 ft 1 in)[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage Height: 2.28 m (7 ft 6 in)[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage Max takeoff weight: 700 kg (1,543 lb)[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage Powerplant: 1 × Thielert Centurion 2.0 diesel engine, 116 kW (155 hp)[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage Main rotor diameter: 7.2 m (23 ft 7 in)[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage Cruise speed: 220 km/h (140 mph, 120 kn)[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage Endurance: 10 hours or >8 hours 100nm (185 km, 115 miles) from the boat.[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage Service ceiling: 6,000 m (20,000 ft)[source]Airbus Helicopters VSR700 · Specifications; only the objects and conditions stated in this passage | — |
|---|
| Country of origin | France[source]Inventory Origin column; table 6, row 4, cell 2; revision 1374114200; retrieved 2026-10-02 | — |
|---|
| Status | — | In production[source] |
|---|
| Manufactured | — | 2018–present[source] |
|---|
| Introduction date | — | January 2018[source] |
|---|
| Battery | — | 11.55V 7100 mAh (82Wh) lithium polymer battery[source] |
|---|
| Camera | — | 20MP 1" CMOS[source] |
|---|
| GNSS compatibility | — | GPS Galileo BeiDou GLONASS[source] |
|---|