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NEX Aero GmbH · Germany
NEX
NEX Aero NEX
升力＋巡航 · 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 seats
- 乘客
- 未公开／未录入
- 驾驶方式
- Piloted at first and autonomous in the future
- 航程（按来源口径）
- Over 400 km (249 miles)
- 巡航速度
- Unknown
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 未公开／未录入
- 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
- Hydrogen fuel cells
- 电机
- 10 electric motors.
- 旋翼／螺旋桨
- 10 propellers (8 dedicated VTOL propellers mounted on booms, 2 tractor propellers mounted on the front of the rear V-tail)
- 续航时间
- Unknown
- 飞行高度
- Unknown
- 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 in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL passenger aircraft
- Piloting
- Piloted at first and autonomous in the future
- Capacity
- 4 seats
- Cruise speed
- Unknown
- Range
- Over 400 km (249 miles)
- Flight time
- Unknown
- Cruise altitude
- Unknown
- Propellers
- 10 propellers (8 dedicated VTOL propellers mounted on booms, 2 tractor propellers mounted on the front of the rear V-tail)
- Electric motors
- 10 electric motors.
- Power source
- Hydrogen fuel cells
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left, right visibility, for spectacular views with a solid roof above the passenger compartment.
- Wings
- 1 main high-wing with winglets
- Tail
- 1 V-tail
- Landing gear
- Tricycle fixed 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 in the sub-systems of the aircraft.