← eVTOL产品
AnTG Industry · China
AnTG One
AnTG Industry AnTG One
多旋翼 · 生产型设计 · 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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot using a three-axis joystick and throttle lever
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 20–40 km/h (12–25 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 150 kg (330 lb)
- 载荷
- 未公开／未录入
- 空重
- 60 kg (132 lb)
- 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
- High-discharge lithium batteries
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers
- 续航时间
- 20 minutes
- 飞行高度
- 5 m (16.4 ft)
- 安全设计
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. 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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL production aircraft
- Piloting
- 1 pilot using a three-axis joystick and throttle lever
- Cruise speed
- 20–40 km/h (12–25 mph)
- Flight time
- 20 minutes
- Maximum altitude
- 5 m (16.4 ft)
- Empty weight
- 60 kg (132 lb)
- Maximum payload weight
- 90 kg (198 lb)
- Maximum takeoff weight
- 150 kg (330 lb)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- High-discharge lithium batteries
- Fuselage
- Carbon fiber composite and aerospace aluminum
- Window
- Open cockpit with roll bars
- Landing gear
- Fixed quadricycle struts or pontoons (has multiple landing gear configurations)
- Safety features
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. 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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.