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Plana · South Korea
CP-01
Plana CP-01
矢量推力 · 阶段未核实 · 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 with room for luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 563 km (350 m)
- 巡航速度
- 300 km/h (186 mph)
- 最大速度
- 350 km/h (217 mph)
- 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
- Hybrid-electric power source
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 tilt-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), 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 in the sub-systems of the aircraft. In an emergency, the aircraft can land like a conventional airplane.
全部原始参数
Specifications:
- Aircraft type
- Medium range hybrid-electric VTOL passenger aircraft
- Piloting
- 1 pilot
- Capacity
- 6 passengers with room for luggage
- Cruise speed
- 300 km/h (186 mph)
- Maximum speed
- 350 km/h (217 mph)
- Range
- 563 km (350 m)
- Propellers
- 6 tilt-propellers
- Electric motors
- 6 electric motors
- Power source
- Hybrid-electric power source
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
- Wings
- 1 front canard wing, 1 rear high main wing
- Tail
- 1 rear vertical stabilizer
- Landing gear
- Retractable tricycle wheeled landing gear
- 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 in the sub-systems of the aircraft. In an emergency, the aircraft can land like a conventional airplane.