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AXIX GP, LLC · USA

SkyRider SUVA

AXIX SkyRider SuvA

多旋翼 · 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 passengers
乘客
未公开/未录入
驾驶方式
1 pilot with A.I. assisted flight controls and satellite navigation
航程(按来源口径)
Unknown
巡航速度
Unknown
最大速度
350 mph (563 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
Hybrid-electric combustion engine
电机
4 electric motors
旋翼/螺旋桨
4 propellers
续航时间
Unknown
飞行高度
30,000 ft (9,144 m)
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. Anti-collision radar. There is a whole aircraft ballistic. The aircraft can also land in water as it has the buoyancy of a boat. parachute.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL passenger aircraft
Piloting
1 pilot with A.I. assisted flight controls and satellite navigation
Capacity
4 passengers
Cruise speed
Unknown
Maximum speed
350 mph (563 km/h)
Range
Unknown
Flight Time
Unknown
Maximum altitude
30,000 ft (9,144 m)
Propellers
4 propellers
Electric Motors
4 electric motors
Power source
Hybrid-electric combustion engine
Fuselage
Carbon fiber composite
Window
Canopy over cockpit, allowing forward, left, right and top visibility, for spectacular views
Landing gear
Retractable strut-type landing gear, located under each propeller. The aircraft can also land in water as it has the buoyancy of a boat.
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. Anti-collision radar. There is a whole aircraft ballistic. The aircraft can also land in water as it has the buoyancy of a boat. parachute.