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SMD Shenzhen Smart Drone UAV Co. Ltd. · China
V800
SMD Shenzhen Smart Drone UAV V800
升力＋巡航 · 生产型设计 · 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
- Air cargo (300 liter capacity)
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 100-120 km/h (62-75 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 220 kg (485 lb)
- 载荷
- 未公开／未录入
- 空重
- 170 kg (375 lb)
- 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
- 5 electric motors
- 旋翼／螺旋桨
- 5 propellers (1 pusher propeller, 4-VTOL propellers)
- 续航时间
- 4-1/2 hours with a full load
- 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 air cargo eVTOL aircraft (production model)
- Piloting
- Remote
- Capacity
- Air cargo (300 liter capacity)
- Cruise speed
- 100-120 km/h (62-75 mph)
- Flight time
- 4-1/2 hours with a full load
- Empty weight
- 170 kg (375 lb)
- Maximum payload weight
- 50 kg (110 lb)
- Maximum takeoff weight
- 220 kg (485 lb)
- Propellers
- 5 propellers (1 pusher propeller, 4-VTOL propellers)
- Electric motors
- 5 electric motors
- Power source
- Battery packs
- Fuselage
- Carbon fiber composite
- Size
- 8200 mm X 3650 mm X 1042 mm (26 ft, 11 in X 12 ft X 3 ft, 5 in)
- Wings
- 1 main high wing
- Tail
- 1 high boom tail (2 vertical stabilizers)
- Landing gear
- Fixed skid 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.