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IO Aircraft · USA
Chippewa 350E
IO Aircraft Chippewa 350E
矢量推力 · 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
- 14 passengers (Can hold a grand total of 16 people, including two pilots)
- 乘客
- 未公开／未录入
- 驾驶方式
- 2 pilots
- 航程（按来源口径）
- 1,151-2,302 miles (1,852-3,705 km)
- 巡航速度
- 345-403 mph (555-649 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 22,000 lb (9,979 kg)
- 载荷
- 10,000 lb (4,536 kg)
- 空重
- 12,000 lb (5,443 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 packs
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 4 propellers
- 续航时间
- Unknown
- 飞行高度
- Unknown
- 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 and the aircraft has a fireproof airframe. In case of an unexpected landing in water, the aircraft fuselage has been designed to float in water. Once landed, the carnard tilt-wings fold against the sides of the fuselage for the safety on people on the ground. The aircraft has a whole aircraft ballistic parachute.
全部原始参数
Specifications:
- Aircraft type
- eVTOL medium class passenger aircraft
- Piloting
- 2 pilots
- Capacity
- 14 passengers (Can hold a grand total of 16 people, including two pilots)
- Cruise speed
- 345-403 mph (555-649 km/h)
- Range
- 1,151-2,302 miles (1,852-3,705 km)
- Flight Time
- Unknown
- Cruise altitude
- Unknown
- Empty weight
- 12,000 lb (5,443 kg)
- Maximum payload
- 10,000 lb (4,536 kg)
- Maximum takeoff weight
- 22,000 lb (9,979 kg)
- Propellers
- 4 propellers
- Electric Motors
- 8 electric motors
- Power source
- Battery packs
- Fuselage
- Graphene composite
- Windows
- Typical sized windows used by convention airplanes
- Wings
- Canard tilt-wings
- Landing gear
- Retractable tricycle twin-wheeled landing gear
- 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 and the aircraft has a fireproof airframe. In case of an unexpected landing in water, the aircraft fuselage has been designed to float in water. Once landed, the carnard tilt-wings fold against the sides of the fuselage for the safety on people on the ground. The aircraft has a whole aircraft ballistic parachute.