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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。
资料覆盖与状态依据
可用性能指标 1/3 · 阶段未核实 · 目录依据 · 目录阶段,尚未核实批准状态
查看状态依据 ↗航程未纳入:单位或条件未能一致解析
订阅本机型报道 RSS →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.
明确提及本机型的报道
暂无明确匹配的公开报道;通用或重名型号不会自动关联。
目录参数变化记录
从保存的目录刷新快照比较,资料修改不等于实机性能发生变化。
暂无已保存的版本变化,后续目录刷新将保留快照。