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Flight Win Innovation Technology Co., Ltd. (Beijing Hangjing Innovation Technology Co., Ltd.) · China
Assault Eagle 2000
Flight Win (Or Flightwin or Beijing Hangjing Innovation Technology) Assault Eagle 2000
矢量推力 · 原型机 · 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 passengers and their luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- >800 km (497 miles)
- 巡航速度
- 未公开／未录入
- 最大速度
- 350 km/h (217 mph)
- 最大起飞重量
- 1,997 kg (4,400 lb)
- 载荷
- 未公开／未录入
- 空重
- 1,497 kg (3,300 lb)
- 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 power source
- 电机
- 2 electric motors
- 旋翼／螺旋桨
- 2 tilt-rotors
- 续航时间
- 未公开／未录入
- 飞行高度
- 未公开／未录入
- 安全设计
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.
全部原始参数
Specifications:
- Aircraft type
- Long-range passenger or air cargo hybrid-electric VTOL tilt-rotor prototype aircraft
- Piloting
- 1 pilot
- Capacity
- 4 passengers and their luggage
- Maximum speed
- 350 km/h (217 mph)
- Range
- >800 km (497 miles)
- Empty weight
- 1,497 kg (3,300 lb)
- Maximum payload weight
- 500 kg (1,100 lb)
- Maximum takeoff weight
- 1,997 kg (4,400 lb)
- Propellers
- 2 tilt-rotors
- Electric motors
- 2 electric motors
- Power source
- Hybrid-electric power source
- Fuselage
- Carbon fiber composite
- Windows
- Larger windows than conventional regional aircraft
- Wings
- 1 high main wing with winglets
- Tail
- 1 V-tail
- Landing gear
- Retractable tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.