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Autonomous Flight · United Kingdom

Y6S

Autonomous Flight Y6S

矢量推力 · 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。

资料覆盖与状态依据

可用性能指标 1/3 · 阶段未核实 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗订阅本机型报道 RSS →

主要参数

座位/载员
2 people including the pilot
乘客
未公开/未录入
驾驶方式
1 pilot (when technology allows, autonomous)
航程(按来源口径)
80 miles (130 km)
巡航速度
未公开/未录入
最大速度
125 mph (201 km/h)
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
Lithium-ion batteries
电机
6 electric motors
旋翼/螺旋桨
6 ducted propellers
续航时间
未公开/未录入
飞行高度
1,500 ft (450 m)
安全设计
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. The aircraft has multiple redundancies, so if there is a single point of failure, other systems are in place so the aircraft will still continue to fly and land safely.

全部原始参数

Specifications:

Aircraft type
eVTOL luxury aircraft
Piloting
1 pilot (when technology allows, autonomous)
Flight controls
Triple redundancy flight controls
Capacity
2 people including the pilot
Maximum speed
125 mph (201 km/h)
Cruise altitude
1,500 ft (450 m)
Range
80 miles (130 km)
Propellers
6 ducted propellers
Electric Motors
6 electric motors
Power source
Lithium-ion batteries
Fuselage
Carbon fiber composite
Windows
Panoramic windows allowing forward, left, right and top visibility, for spectacular views
Wings
Canard low front wing and a high rear wing. The rear high wing has winglets.
Landing gear
Fixed skid-type landing gear. The full-scale prototype has tricycle type fixed-landing legs with 2 additional legs, one leg near the end of each of the forward canard wings.
Safety Features
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. The aircraft has multiple redundancies, so if there is a single point of failure, other systems are in place so the aircraft will still continue to fly and land safely.

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。