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IO Aircraft · USA

Skyline-H

IO Aircraft Skyline-H

多旋翼 · 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
1 passenger
乘客
未公开/未录入
驾驶方式
Autonomous with manual flying option
航程(按来源口径)
Unknown
巡航速度
288 mph (463 km/h)
最大速度
未公开/未录入
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, hydrogen fuel cell stacks
电机
8 electric motors
旋翼/螺旋桨
4 propellers
续航时间
Unknown
飞行高度
10,000 ft (3,048 m)
安全设计
Has eight electric motors, if one or two electric motors fail, the other electric motors can handle landing the aircraft safely. There are multiple redundant avionics and electrical systems, the aircraft has a fireproof airframe and there is a whole aircraft ballistic parachute system. In case of an unexpected landing in water, the aircraft fuselage has been designed to float in water. There is a lithium battery backup providing five minutes for the aircraft providing time to land the aircraft safely. Once landed, the propeller nacelles fold against the sides of the fuselage for the safety on people on the ground.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL passenger aircraft
Piloting
Autonomous with manual flying option
Capacity
1 passenger
Cruise speed
288 mph (463 km/h)
Range
Unknown
Flight Time
Unknown
Maximum altitude
10,000 ft (3,048 m)
Propellers
4 propellers
Electric Motors
8 electric motors
Power source
Hybrid-electric, hydrogen fuel cell stacks
Fuselage
Graphene composite fuselage
Windows
Canopy over cockpit allowing forward, left, right and top visibility, for spectacular views
Landing gear
Fixed tricycle landing gear, with one wheel in the front and two wheels in the rear of the aircraft
Safety features
Has eight electric motors, if one or two electric motors fail, the other electric motors can handle landing the aircraft safely. There are multiple redundant avionics and electrical systems, the aircraft has a fireproof airframe and there is a whole aircraft ballistic parachute system. In case of an unexpected landing in water, the aircraft fuselage has been designed to float in water. There is a lithium battery backup providing five minutes for the aircraft providing time to land the aircraft safely. Once landed, the propeller nacelles fold against the sides of the fuselage for the safety on people on the ground.