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Vertaxi · China
Matrix 1
Vertaxi Matrix 1
升力＋巡航 · 原型机 · 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
- 5 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote, autopilot or autonomous piloting
- 航程（按来源口径）
- 250 km (155 m)
- 巡航速度
- 200 km/h (123 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 2,000 kg (4,409 lb)
- 载荷
- 500 kg (1,102 lb)
- 空重
- 1,500 kg (3,307 lb)
- 长度
- 未公开／未录入
- 翼展
- 15 m (49 ft, 2-1/2 in)
- 高度
- 未公开／未录入
- 动力来源
- Batteries
- 电机
- 20 electric motors
- 旋翼／螺旋桨
- 20 propellers. 4 tractor propellers, for forward flight, and 16 VTOL propellers. All propellers are mounted on the four booms attached to the main high wing and tail.
- 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 of critical components in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Passenger and air cargo eVTOL prototype aircraft
- Piloting
- Remote, autopilot or autonomous piloting
- Capacity
- 5 passengers
- Cruise speed
- 200 km/h (123 mph)
- Range
- 250 km (155 m)
- Empty weight
- 1,500 kg (3,307 lb)
- Maximum payload
- 500 kg (1,102 lb)
- Maximum takeoff weight
- 2,000 kg (4,409 lb)
- Propellers
- 20 propellers. 4 tractor propellers, for forward flight, and 16 VTOL propellers. All propellers are mounted on the four booms attached to the main high wing and tail.
- Electric motors
- 20 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left, right and top visibility for spectacular views with a solid roof above the passenger compartment
- Wings
- 1 main high-wing with winglets
- Wing span
- 15 m (49 ft, 2-1/2 in)
- Tail
- 1 modified elongated tail with a V forming from the fuselage. At the top of the V tail are short horizontal wings with winglets.
- Landing gear
- Fixed tricycle landing struts
- 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 of critical components in the sub-systems of the aircraft.