跳到正文
← eVTOL产品

AutoFlight · China

Prosperity

AutoFlight Prosperity V2000EM

升力+巡航 · 生产型设计 · 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
4 passengers and their luggage
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
250 km (155 m)
巡航速度
200 km/h (124 mph)
最大速度
未公开/未录入
最大起飞重量
2,220 kg (4,894 lb)
载荷
未公开/未录入
空重
1,870 kg (4,122 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
Battery packs
电机
13 electric motors
旋翼/螺旋桨
13 propellers (10 VTOL only propellers, 3 pusher propellers)
续航时间
未公开/未录入
飞行高度
未公开/未录入
安全设计
Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. 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 aircraft (production model)
Piloting
1 pilot
Capacity
4 passengers and their luggage
Cruise speed
200 km/h (124 mph)
Range
250 km (155 m)
Empty weight
1,870 kg (4,122 lb)
Maximum payload weight
350 kg (772 lb)
Maximum takeoff weight
2,220 kg (4,894 lb)
Propellers
13 propellers (10 VTOL only propellers, 3 pusher propellers)
Electric motors
13 electric motors
Power source
Battery packs
Fuselage
Carbon fiber composite
Windows
Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
Wings
1 canard. 1 high gull wing. 4 booms for VTOL propellers.
Tail
2 downward vertical stabilizers
Landing gear
Fixed skid landing gear
Safety features
Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. 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.