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Volkswagen Group China · China
V.MO Sky Garden
Volkswagen Group China V.MO Sky Garden
升力+巡航 · 阶段未核实 · 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
- 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)
- 200 km (124 miles).
- 巡航速度
- 未公开/未录入
- 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
- 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
- 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
- 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. There are also redundancies in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- eVTOL flying prototype passenger aircraft
- Piloting
- Remote or autonomous. The production aircraft will be fully autonomous.
- Capacity
- 4 passengers
- Range
- 200 km (124 miles).
- Flight time
- 60 minutes
- Propellers
- 10 propellers (8 VTOL propellers, 2 pusher propellers)
- Electric motors
- 10 electric motors
- Power source
- Swappable battery packs
- Fuselage
- Carbon fiber composite
- Windows
- 1 large forward window and 2 long and tall side windows and a sun roof, for spectacular views for the passengers
- Wings
- Tandem 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.