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Voltline · South Korea
Skyla_V2
Voltline Skyla_V2
多旋翼 · 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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot (manually piloted, by autopilot or by remote control)
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 60-90 km/h (37-56 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 300 kg (660 lb)
- 载荷
- 150 kg (330 lb)
- 空重
- 150 kg (330 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
- Lithium polymer batteries
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers
- 续航时间
- 20 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 of critical components in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- eVTOL one passenger multicopter production aircraft
- Piloting
- 1 pilot (manually piloted, by autopilot or by remote control)
- Cruise speed
- 60-90 km/h (37-56 mph)
- Flight time
- 20 minutes
- Empty weight
- 150 kg (330 lb)
- Maximum payload
- 150 kg (330 lb)
- Maximum takeoff weight
- 300 kg (660 lb)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Lithium polymer batteries
- Dimensions
- 2,400 mm X 2,667 mm X 2,627 mm (7.78 feet X 8.75 feet X 8.62 feet)
- Fuselage
- Open framework fuselage made of aluminum, fiber-reinforced plastic and carbon fiber composite
- Landing gear
- Lands on the bottom frame of the fuselage
- 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 of critical components in the sub-systems of the aircraft.