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SeaplaneX
Seaplane Hong Kong Group SeaplaneX
矢量推力 · 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。
资料覆盖与状态依据
可用性能指标 2/3 · 概念设计 · 目录依据 · 目录阶段,尚未核实批准状态
查看状态依据 ↗概念参数,尚不代表已实现性能
订阅本机型报道 RSS →主要参数
- 座位/载员
- 8 passengers
- 乘客
- 未公开/未录入
- 驾驶方式
- Autonomous
- 航程(按来源口径)
- 400 km (249 m)
- 巡航速度
- ~80-260 km/h (~50-162 mph), or possibly faster
- 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 and battery packs
- 电机
- 4 electric motors
- 旋翼/螺旋桨
- 4 propellers
- 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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
全部原始参数
Specifications:
- Aircraft type
- Scalable passenger hydrogen-electric VTOL concept design aircraft
- Piloting
- Autonomous
- Capacity
- 8 passengers
- Cruise speed
- ~80-260 km/h (~50-162 mph), or possibly faster
- Maximum range
- 400 km (249 m)
- Maximum payload weight
- 1,000 kg (2,205 lb)
- Propellers
- 4 propellers
- Electric motors
- 4 electric motors
- Power source
- Hydrogen fuel cells and battery packs
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
- Wings
- 1 main high wing
- Tail
- 1 V-tail
- Landing gear
- Retractable tricycle dual-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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
明确提及本机型的报道
暂无明确匹配的公开报道;通用或重名型号不会自动关联。
目录参数变化记录
从保存的目录刷新快照比较,资料修改不等于实机性能发生变化。
暂无已保存的版本变化,后续目录刷新将保留快照。