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Rictor, KuickWheel · China
Skyrider X1
Rictor, KuickWheel Skyrider X1
个人飞行器 · 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 with an AI automatic route planning function and automated takeoff and landing capability. The company's avionics adjusts flight altitude, speed and direction in real-time according to weather and environmental changes, for an efficient and safe flight experience. The aircraft can be flown manually with a joystick control. Displays real-time data, weather updates, and system status for full situational awareness.
- 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
- 200 kg (440 lb)
- 载荷
- 未公开/未录入
- 空重
- 80 kg (176 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
- Hybrid-electric power source
- 电机
- 8 electric motors
- 旋翼/螺旋桨
- 8 stacked propellers (with automatic folding and unfolding system)
- 续航时间
- 25-40 minutes
- 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. Specifically, the aircraft has a triple-redundant flight control system. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
全部原始参数
Specifications:
- Aircraft type
- Passenger hybrid-electric VTOL sea-land-air motorcycle-aircraft
- Piloting
- 1 pilot with an AI automatic route planning function and automated takeoff and landing capability. The company's avionics adjusts flight altitude, speed and direction in real-time according to weather and environmental changes, for an efficient and safe flight experience. The aircraft can be flown manually with a joystick control. Displays real-time data, weather updates, and system status for full situational awareness.
- Maximum cruise speed
- 100 km/h (62 mph)
- Range (air)
- 300 km (186 miles)
- Flight time
- 25-40 minutes
- Maximum cruise altitude
- 200 m (656 ft)
- Empty weight
- 80 kg (176 lb)
- Maximum payload weight
- 120 kg (264 lb)
- Maximum takeoff weight
- 200 kg (440 lb)
- Propellers
- 8 stacked propellers (with automatic folding and unfolding system)
- Electric motors
- 8 electric motors
- Power source
- Hybrid-electric power source
- Fuselage
- Carbon fiber composite and aerospace-grade aluminum
- Window
- Canopy over cockpit
- Landing gear
- Retractable 1 front and 1 rear motorcycle tires, with retractable rear training wheels to keep the flying motorcycle upright without having to use a kickstand
- 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. Specifically, the aircraft has a triple-redundant flight control system. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.