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Aerial Rider · China
5A 01, 03, 06, 09 Series
Aerial Rider 5A Series
电动旋翼机 · 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
- Air cargo, agricultural spraying, surveillance and more
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote, autopilot or autonomous
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- Unknown
- 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
- Has multiple engine configurations, such as using a turboshaft engine, hybrid or hydrogen technologies
- 电机
- 未公开／未录入
- 旋翼／螺旋桨
- 1 main rotorblade with three rotorblades
- 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) 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.
全部原始参数
Specifications:
- Aircraft type
- Scalable uncrewed multirole air cargo helicopter
- Piloting
- Remote, autopilot or autonomous
- Capacity
- Air cargo, agricultural spraying, surveillance and more
- Cruise speed
- Unknown
- 5A01 maximum takeoff weight
- 120 kg (265 lb)
- 5A03 maximum takeoff weight
- 180 kg (397 lb)
- 5A06 maximum takeoff weight
- 125 kg (276 lb)
- 5A09 maximum takeoff weight
- 760 kg (1,676 lb)
- Propellers
- 1 main rotorblade with three rotorblades
- Tail rotor
- 1 tail rotor
- Power source
- Has multiple engine configurations, such as using a turboshaft engine, hybrid or hydrogen technologies
- Fuselage
- Carbon fiber composite
- Landing gear
- Fixed skid landing gear
- 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.