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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
No passengers
乘客
未公开/未录入
驾驶方式
Autonomous piloting
航程(按来源口径)
未公开/未录入
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
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
未公开/未录入
旋翼/螺旋桨
未公开/未录入
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) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure.

全部原始参数

Specifications:

Aircraft type
eVTOL roadable fully functional ¼ subscale prototype vehicle
Piloting
Autonomous piloting
Capacity
No passengers
Cruise speed
Unknown
Empty weight (passenger capsule and drone module)
~45 kg (~100 lb)
Propellers (drone module)
8 propellers
Electric motors (drone module)
8 electric motors
Ground wheels (ground module)
4 ground wheels
Electric motors (ground module)
4 electric motors
Power source
Battery packs
Passenger Fuselage (capsule)
Unknown
Road chassis material
Unknown
Landing gear
The drone module lands the passenger capsule onto the ground vehicle chassis
Safety features
Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure.