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China Automotive Innovation Corporation (CAIC) · China

Jiangtun 1

China Automotive Innovation Corporation (CAIC) Jiangtun 1

矢量推力 · 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
No passenger or cargo hold
乘客
未公开/未录入
驾驶方式
Remote piloting, possibly AI flight control systems
航程(按来源口径)
未公开/未录入
巡航速度
120 km/h (75 mph)
最大速度
未公开/未录入
最大起飞重量
未公开/未录入
载荷
未公开/未录入
空重
未公开/未录入
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
Battery packs
电机
8 electric motors
旋翼/螺旋桨
8 propellers (4 VTOL-only propellers, 4 tilt-propellers)
续航时间
未公开/未录入
飞行高度
100 m (328 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.

全部原始参数

Specifications:

Aircraft type
Uncrewed eVTOL subscale prototype
Piloting
Remote piloting, possibly AI flight control systems
Capacity
No passenger or cargo hold
Cruise speed
120 km/h (75 mph)
Cruise altitude
100 m (328 ft)
Maximum payload weight (estimated)
170 kg (375 lb)
Propellers
8 propellers (4 VTOL-only propellers, 4 tilt-propellers)
Electric motors
8 electric motors
Power source
Battery packs
Fuselage
Carbon fiber composite
Wings
1 high main wing
Tail
V tail
Landing gear
Fixed tricycle landing struts
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.