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Volkswagen Group China · China

V.MO Flying Tiger (Prototype 1)

Volkswagen Group China V.MO Flying Tiger (Prototype 1)

升力+巡航 · 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
0 passengers. The production aircraft will carry 4 passengers.
乘客
未公开/未录入
驾驶方式
Remote or autonomous. The production aircraft will be fully autonomous.
航程(按来源口径)
Unknown. The production aircraft's estimated range is 200 km (124 miles).
巡航速度
Unknown
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
未公开/未录入
长度
11.2 meters (36.7 feet)
翼展
未公开/未录入
高度
未公开/未录入
动力来源
Swappable battery packs
电机
10 electric motors
旋翼/螺旋桨
10 propellers (8 VTOL propellers, 2 pusher propellers)
续航时间
60 minutes
飞行高度
Unknown
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. There are also redundancies in the sub-systems of the aircraft.

全部原始参数

Specifications:

Aircraft type
eVTOL flying subscale prototype passenger aircraft
Piloting
Remote or autonomous. The production aircraft will be fully autonomous.
Capacity
0 passengers. The production aircraft will carry 4 passengers.
Cruise speed
Unknown
Range
Unknown. The production aircraft's estimated range is 200 km (124 miles).
Flight time
60 minutes
Cruise altitude
Unknown
Propellers
10 propellers (8 VTOL propellers, 2 pusher propellers)
Electric motors
10 electric motors
Power source
Swappable battery packs
Fuselage
Carbon fiber composite
Length
11.2 meters (36.7 feet)
Width
10.6 meters (34.7 feet)
Windows
None
Wings
Canard high-wings
Landing gear
Fixed skid-type 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. There are also redundancies in the sub-systems of the aircraft.