跳到正文
← eVTOL产品

UDX Research s.r.o. · 未公开/未录入

Airwolf

UDX Research Airwolf

个人飞行器 · 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 ↗

航程含设计目标/上限条件

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
1 passenger
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
Up to 66 km (41 m)
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
440 kg (969 lb)
载荷
未公开/未录入
空重
290 kg (639 lb)
长度
3.2 m (10 ft, 6 in)
翼展
未公开/未录入
高度
未公开/未录入
动力来源
Battery packs
电机
4 electric motors
旋翼/螺旋桨
4 electric ducted fans (EDFs)
续航时间
~25 minutes
飞行高度
未公开/未录入
安全设计
Distributed electric propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. 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
Passenger eVTOL concept design hoverbike
Piloting
1 pilot
Capacity
1 passenger
Maximum cruise speed
230 km/h (143 mph)
Acceleration
0-100 km/h: 3 seconds (0-62 mph: 3 seconds)
Range
Up to 66 km (41 m)
Flight time
~25 minutes
Empty weight
290 kg (639 lb)
Maximum payload weight
150 kg (330 lb)
Maximum takeoff weight
440 kg (969 lb)
Propellers
4 electric ducted fans (EDFs)
Electric motors
4 electric motors
Power source
Battery packs
Fuselage
Carbon fiber composite
Flight width
4.55 m (14 ft, 11.25 in)
Transport width
2.45 m (8 ft, 1/2 in)
Length
3.2 m (10 ft, 6 in)
Window
Open cockpit
Wings
Tandem wings
Landing gear
Lands on the bottom of its fuselage
Safety features
Distributed electric propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. 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.

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。