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SMD Shenzhen Smart Drone UAV Co. Ltd. · China

V3000

SMD Shenzhen Smart Drone UAV V3000

矢量推力 · 概念设计 · 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
6 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)
500 km (311 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
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
Hydrogen fuel cells and lithium battery packs
电机
6 electric motors
旋翼/螺旋桨
6 propellers (2 tilt-propellers, 4-VTOL only 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.

全部原始参数

Specifications:

Aircraft type
Long-range passenger hydrogen-fuel cell eVTOL aircraft (concept design)
Piloting
1 pilot
Capacity
6 passengers and their luggage
Cruise speed
Unknown
Range
500 km (311 miles)
Propellers
6 propellers (2 tilt-propellers, 4-VTOL only propellers)
Electric motors
6 electric motors
Power source
Hydrogen fuel cells and lithium battery packs
Fuselage
Carbon fiber composite
Windows
Larger than conventional aircraft
Wings
Tandem wings with winglets
Tail
1 vertical stabilizer
Landing gear
Retractable tricycle wheeled 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.