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IO Aircraft · USA
Hornet
IO Aircraft Hornet
个人飞行器 · 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 or piloted optional
- 航程（按来源口径）
- 50 miles (80 km)
- 巡航速度
- 63 mph (101 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 265 lb (120 kg)
- 载荷
- 250 lb (113 kg)
- 空重
- 125 lb (57 kg)
- 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
- Battery pack
- 电机
- 4 electric motors
- 旋翼／螺旋桨
- 2 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
- Has four 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.
全部原始参数
Specifications:
- Aircraft type
- eVTOL personal back-pack flying device
- Piloting
- Autonomous or piloted optional
- Capacity
- 1 passenger
- Cruise speed
- 63 mph (101 km/h)
- Range
- 50 miles (80 km)
- Empty weight
- 125 lb (57 kg)
- Maximum payload
- 250 lb (113 kg)
- Maximum takeoff weight
- 265 lb (120 kg)
- Propellers
- 2 propellers
- Electric Motors
- 4 electric motors
- Power source
- Battery pack
- Fuselage
- Graphene composite fuselage
- Landing gear
- Fixed landing legs
- Safety features
- Has four 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.