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IO Aircraft · USA
Challenger SC
IO Aircraft Challenger SC
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
- 5 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 920 miles (1,480 km)
- 巡航速度
- 287 mph (462 km/h) below 10,000 ft (3,048 m). 460 mph (740 km/h) when above 10,000 ft (3,048 m).
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 5,000 lb (2,268 kg)
- 载荷
- 2,000 lb (907 kg)
- 空重
- 3,000 lb (1,361 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
- Hydrogen fuel cells
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 electric ducted fans
- 续航时间
- 未公开／未录入
- 飞行高度
- 20,000 ft (6,096 km)
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft. Crash survivability include a Ballistic Recovery System (BRS), 5G crush resistance and the seats incorporate a scissor suspension system which in case of a hard landing or failure, will provide enormous shock absorption for the passengers.
全部原始参数
Specifications:
- Aircraft type
- High-performance hybrid-electric VTOL passenger aircraft
- Piloting
- 1 pilot
- Capacity
- 5 passengers
- Cruise speed
- 287 mph (462 km/h) below 10,000 ft (3,048 m). 460 mph (740 km/h) when above 10,000 ft (3,048 m).
- Range
- 920 miles (1,480 km)
- Maximum altitude
- 20,000 ft (6,096 km)
- Empty weight
- 3,000 lb (1,361 kg)
- Maximum payload
- 2,000 lb (907 kg)
- Maximum takeoff weight
- 5,000 lb (2,268 kg)
- Propellers
- 8 electric ducted fans
- Electric Motors
- 8 electric motors
- Power source
- Hydrogen fuel cells
- Fuselage
- Graphene composite
- 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
- Wings
- Tandem wings
- Landing gear
- Retractable tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft. Crash survivability include a Ballistic Recovery System (BRS), 5G crush resistance and the seats incorporate a scissor suspension system which in case of a hard landing or failure, will provide enormous shock absorption for the passengers.