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Honda · Japan
Honda eVTOL
Honda eVTOL
升力＋巡航 · 概念设计 · 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）
- 未公开／未录入
- 巡航速度
- 未公开／未录入
- 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
- Gas turbine hybrid-electric power source
- 电机
- 10 electric motors
- 旋翼／螺旋桨
- 未公开／未录入
- 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 enhance 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
- Hybrid-electric VTOL
- Piloting
- 1 pilot
- Capacity
- 4 passengers and their luggage
- Range (estimated)
- 400 km (250 m)
- VTOL propellers
- 8 VTOL propellers
- Forward flight propellers
- 2 propellers for forward flight
- Electric motors
- 10 electric motors
- Power source
- Gas turbine hybrid-electric power source
- Windows
- The aircraft has taller windows than most standard aircraft, for spectacular views for the passengers
- Fuselage
- Carbon fiber composite
- Wings
- Two high tandem wings with winglets and with booms parallel to the fuselage to hold the VTOL propellers
- Tail
- There is no tail for the aircraft but there are two vertical stabilizers at the end of the rear wing, near the rear of the aircraft
- 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 enhance 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.