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Vision Aeronautics · China

Vector 5

Vision Aeronautics Vector 5

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。

资料覆盖与状态依据

可用性能指标 1/3 · 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 ↗

巡航速度未纳入:单位或条件未能一致解析

概念参数,尚不代表已实现性能

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主要参数

座位/载员
7 passengers
乘客
未公开/未录入
驾驶方式
Unknown
航程(按来源口径)
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
3,000 kg (6,614 lbs)
载荷
未公开/未录入
空重
2320 kg (5,115 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
Battery packs
电机
11 electric motors
旋翼/螺旋桨
8 VTOL-only propellers, 3 pusher 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. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity. In an emergency, the aircraft can land conventionally if the VTOL propellers stop working.

全部原始参数

Specifications:

Aircraft type
Passenger eVTOL concept design aircraft
Piloting
Unknown
Capacity
7 passengers
Cruise speed
Unknown
Range
400 km (249 miles)
Empty weight
2320 kg (5,115 lb)
Maximum payload weight
680 kg (1,499 lbs)
Maximum takeoff weight
3,000 kg (6,614 lbs)
Propellers
8 VTOL-only propellers, 3 pusher propellers
Electric motors
11 electric motors
Power source
Battery packs
Fuselage
More than 60% carbon fiber composite
Dimensions
Wingspan 15.5 meters (51 feet), fuselage length 11 meters (36 feet)
Windows
Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with see-through roof above the passenger compartment
Wings
1 high main gull-wing
Tail
Conventional tail
Landing gear
Fixed 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. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity. In an emergency, the aircraft can land conventionally if the VTOL propellers stop working.

明确提及本机型的报道

7月25日周六
2025年6月20日周五

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。