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IO Aircraft · USA
Aelous
IO Aircraft Aelous
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
- 4-5 passengers (If in autonomous mode, 5 passenger.), plus dual baggage compartments
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot with 4 passengers or autonomous
- 航程（按来源口径）
- 450-550 miles (724-885 km)
- 巡航速度
- 172-368 mph (277-592 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 2,100 lb (952 kg)
- 载荷
- 1,200 lb (544 kg)
- 空重
- 900 lb (408 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
- Hybrid-electric, hydrogen fuel cells
- 电机
- 8 electric motors, 180+ SHP each
- 旋翼／螺旋桨
- 4 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 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.
全部原始参数
Specifications:
- Aircraft type
- High-performance hybrid-electric VTOL passenger aircraft
- Piloting
- 1 pilot with 4 passengers or autonomous
- Capacity
- 4-5 passengers (If in autonomous mode, 5 passenger.), plus dual baggage compartments
- Cruise speed
- 172-368 mph (277-592 km/h)
- Range
- 450-550 miles (724-885 km)
- Empty weight
- 900 lb (408 kg)
- Maximum payload
- 1,200 lb (544 kg)
- Maximum takeoff weight
- 2,100 lb (952 kg)
- Propellers
- 4 propellers
- Electric Motors
- 8 electric motors, 180+ SHP each
- Power source
- Hybrid-electric, hydrogen fuel cells
- Fuselage
- Graphene composite fuselage
- Windows
- Larger than normal aircraft windows allowing forward, left, right visibility, for spectacular views and the aircraft has a solid roof above the passenger compartment
- Landing gear
- Retractable 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.