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Airbus Helicopters · Germany

CityAirbus NextGen

Airbus Helicopters CityAirbus NextGen

多旋翼 · 原型机 · 核查 2026-10-01

下列为 VFS 目录披露的参数,包含设计目标及历史版本信息。目录阶段不等于适航或量产状态;不同任务条件的航程与载荷不能直接当作同一条件下的性能。

主要参数

座位/载员
3 passengers and their luggage
乘客
未公开/未录入
驾驶方式
1 pilot (Piloted initially and will become autonomous when regulations allow)
航程(按来源口径)
80 km (50 miles)
巡航速度
120 km/h (75 mph)
最大速度
未公开/未录入
最大起飞重量
未公开/未录入
载荷
未公开/未录入
空重
2,000 kg (4,409 lb)
长度
未公开/未录入
翼展
未公开/未录入
高度
未公开/未录入
动力来源
Batteries
电机
16 electric motors (16 electric motors for redundancy, that is, for safety)
旋翼/螺旋桨
8 propellers (each propeller has four propeller blades)
续航时间
Unknown
飞行高度
未公开/未录入
安全设计
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.

全部原始参数

Specifications:

Aircraft type
Passenger eVTOL prototype aircraft
Piloting
1 pilot (Piloted initially and will become autonomous when regulations allow)
Capacity
3 passengers and their luggage
Cruise speed
120 km/h (75 mph)
Range
80 km (50 miles)
Flight Time
Unknown
Empty weight
2,000 kg (4,409 lb)
Propellers
8 propellers (each propeller has four propeller blades)
Electric Motors
16 electric motors (16 electric motors for redundancy, that is, for safety)
Power source
Batteries
Fuselage
Carbon fiber composite
Windows
Large front windscreen and each door has windows
Wing
1 high forward-swept wing, 12 m (~39 ft, 4-3/8 in)
Tail
1 double-boom mounted shallow U-shaped tail
Landing gear
Fixed skid landing gear
Safety features
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.