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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。
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.