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IO Aircraft · USA
Chippewa 350M
IO Aircraft Chippewa 350M
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
- 20 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 3 crew
- 航程（按来源口径）
- 1,151 miles (1,852 km) fuel or fuel cells / 2,302 miles (3,704 km) using both fuel and fuel cells
- 巡航速度
- 401 mph (249 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
- 6,000-8,000 lb (2,722-3,629 kg)
- 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
- 88 hydrogen fuel cells and 2 turbine engines using petroleum fuel, making the aircraft have dual power sources
- 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 canard tilt-wings fold against the sides of the fuselage for the safety on people on the ground.
全部原始参数
Specifications:
- Aircraft type
- eVTOL medium class passenger aircraft
- Piloting
- 3 crew
- Capacity
- 20 passengers
- Cruise speed
- 401 mph (249 km/h)
- Range
- 1,151 miles (1,852 km) fuel or fuel cells / 2,302 miles (3,704 km) using both fuel and fuel cells
- Flight Time
- Unknown
- Cruise altitude
- Unknown
- Maximum payload
- 6,000-8,000 lb (2,722-3,629 kg)
- Doors
- 2 large front doors, 1 rear bay payload door
- Propellers
- 4 propellers
- Electric Motors
- 8 electric motors
- Turbines
- 2 turbine like nacelles on the top rear of the aircraft
- Power source
- 88 hydrogen fuel cells and 2 turbine engines using petroleum fuel, making the aircraft have dual power sources
- 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 canard tilt-wings fold against the sides of the fuselage for the safety on people on the ground.