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AIR VEV Ltd · Israel
AIR ONE
AIR VEV AIR ONE
矢量推力 · 技术验证机 · 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
- 2 passengers, pilot and passenger
- 乘客
- 未公开／未录入
- 驾驶方式
- 未公开／未录入
- 航程（按来源口径）
- 未公开／未录入
- 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
- 2,688 lb (1,220 kg)
- 载荷
- 未公开／未录入
- 空重
- 2,138 lb (970 kg)
- 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
- Batteries
- 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
- 未公开／未录入
- 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. Having multiple redundant systems on any aircraft decreases having any single point of failure. If for some reason, all propellers stop working, the aircraft can also land conventionally on runway or road. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL technology demonstrator aircraft
- Capacity
- 2 passengers, pilot and passenger
- Cruise Speed (estimated)
- 155 mph (249 km/h)
- Range (estimated)
- 110 mi (177 km)
- Empty weight
- 2,138 lb (970 kg)
- Maximum payload weight
- 550 lb (250 kg)
- Maximum takeoff weight
- 2,688 lb (1,220 kg)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Batteries
- Windows
- Canopy over cockpit
- Wing
- 1 main high-wing
- Tail
- Boom mounted vertical stabilizers
- Landing gear
- Fixed quadricycle wheeled 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. There are also redundancies in the sub-systems of the aircraft. Having multiple redundant systems on any aircraft decreases having any single point of failure. If for some reason, all propellers stop working, the aircraft can also land conventionally on runway or road. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.