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Aerial Rider · China
1A Series
Aerial Rider 1A Series
升力＋巡航 · 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。
资料覆盖与状态依据
可用性能指标 0/3 · 生产型设计 · 目录依据 · 目录阶段，尚未核实批准状态
查看状态依据 ↗航程未纳入：单位或条件未能一致解析
巡航速度未纳入：单位或条件未能一致解析
订阅本机型报道 RSS →主要参数
- 座位／载员
- Sensor equipment, cameras or air cargo
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote or autonomous
- 航程（按来源口径）
- Long-range aircraft
- 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
- Hybrid-electric power source (there could be an all batteries power source option)
- 电机
- 5 electric motors
- 旋翼／螺旋桨
- 5 propellers (4 VTOL-only propellers, 1 pusher propeller)
- 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.
全部原始参数
Specifications:
- Aircraft type
- Surveillance and air cargo hybrid-electric VTOL production model aircraft
- Piloting
- Remote or autonomous
- Capacity
- Sensor equipment, cameras or air cargo
- Cruise speed
- Unknown
- Range
- Long-range aircraft
- Maximum payload weight
- Unknown
- Propellers
- 5 propellers (4 VTOL-only propellers, 1 pusher propeller)
- Electric motors
- 5 electric motors
- Power source
- Hybrid-electric power source (there could be an all batteries power source option)
- Fuselage
- Carbon fiber composite
- Wing
- 1 main wing with winglets
- Tail
- 1 horizontal stabilizer
- Landing gear
- Unknown
- 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.
明确提及本机型的报道
暂无明确匹配的公开报道；通用或重名型号不会自动关联。
目录参数变化记录
从保存的目录刷新快照比较，资料修改不等于实机性能发生变化。
暂无已保存的版本变化，后续目录刷新将保留快照。