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Airbus Acubed · USA
Vahana Alpha Two
Airbus Acubed Vahana Alpha Two
矢量推力 · 停研／历史型号 · 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
- There is a seat for 1 passenger, the cockpit instrument panel is a mock-up
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote controlled
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 125 mph (200 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 1,800 lb (816 kg)
- 载荷
- 200 lb (90 kg)
- 空重
- 1,600 lb (726 kg)
- 长度
- 未公开／未录入
- 翼展
- 20.6 ft (6.25 m)
- 高度
- 未公开／未录入
- 动力来源
- Battery packs
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers
- 续航时间
- 未公开／未录入
- 飞行高度
- 5,000 ft (1,524 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.
全部原始参数
Specifications:
- Aircraft type
- eVTOL trade show mock-up
- Piloting
- Remote controlled
- Capacity
- There is a seat for 1 passenger, the cockpit instrument panel is a mock-up
- Cruise speed
- 125 mph (200 km/h)
- Range with reserves
- 30 miles (50 km)
- Cruise altitude
- 5,000 ft (1,524 m)
- Empty weight
- 1,600 lb (726 kg)
- Maximum payload
- 200 lb (90 kg)
- Maximum takeoff weight
- 1,800 lb (816 kg)
- Propellers
- 8 propellers
- Electric Motors
- 8 electric motors
- Motor output
- 8 x 60 hp (8 x 45 kw)
- Power source
- Battery packs
- Fuselage
- Carbon fiber composite
- Fuselage length
- 19.5 ft (5.86 m)
- Overall height
- 9.275 ft (2.81 m)
- Wingspan
- 20.6 ft (6.25 m)
- Tip-to-tip distance
- 19.69 ft (6 m )
- Windows
- Canopy over cockpit
- Wings
- Canard tilt-wing, each wing can tilt independently
- Landing gear
- Fixed skid-type landing gear
- 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.