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Volocopter GmbH · Germany

e-volo uVC200 cargo

Volocopter e-volo uVC200 cargo

多旋翼 · 停研/历史型号 · 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。

资料覆盖与状态依据

可用性能指标 1/3 · 停研/历史型号 · 目录阶段,尚未核实批准状态

查看状态依据 ↗订阅本机型报道 RSS →

主要参数

座位/载员
Cargo only, no passengers
乘客
未公开/未录入
驾驶方式
Remote or autonomous
航程(按来源口径)
未公开/未录入
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
200 kg (441 lb)
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 or hybrid-electric power source
电机
18 electric motors
旋翼/螺旋桨
18 propellers
续航时间
30 minutes with a battery-only power source, 4 hours with a hybrid-electric power source
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 and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. There is also an aircraft parachute. Has automatic altitude control, automatic gentle landing, crosswinds and turbulence is automatically compensated for. Redundancy has been built into the aircraft so if one critical system breaks, there are other same exact systems so the aircraft can continue flying and safely land.

全部原始参数

Specifications:

Aircraft type
eVTOL or hybrid-electric VTOL cargo design concept
Piloting
Remote or autonomous
Capacity
Cargo only, no passengers
Flight time
30 minutes with a battery-only power source, 4 hours with a hybrid-electric power source
Maximum payload
200 kg (441 lb)
Propellers
18 propellers
Electric Motors
18 electric motors
Propeller frame assembly diameter
5.4 meters (over 17-1/2 feet)
Fuselage
Based on the e-volo VC200 single passenger eVTOL aircraft
Power source
Battery or hybrid-electric power source
Landing gear
Fixed skid landing gear
Safety Features
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. There is also an aircraft parachute. Has automatic altitude control, automatic gentle landing, crosswinds and turbulence is automatically compensated for. Redundancy has been built into the aircraft so if one critical system breaks, there are other same exact systems so the aircraft can continue flying and safely land.

明确提及本机型的报道

暂无明确匹配的公开报道;通用或重名型号不会自动关联。

目录参数变化记录

从保存的目录刷新快照比较,资料修改不等于实机性能发生变化。

暂无已保存的版本变化,后续目录刷新将保留快照。

公司资料与事件

包括公司融资及其他机型进展,请查看原文确认涉及的具体型号。

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