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Hongqi · China
Sky Sedan 1
Hongqi Sky Sedan 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
- 1 passenger and luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot and luggage
- 航程（按来源口径）
- 200 km (124 miles)
- 巡航速度
- 150 km/h (93 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 (most likely)
- 电机
- 10 electric motors for the flight module
- 旋翼／螺旋桨
- 2 pusher propellers, 8 VTOL-only propellers
- 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
- Modular passenger eVTOL air/ground prototype vehicle
- Piloting
- 1 pilot and luggage
- Capacity
- 1 passenger and luggage
- Cruise speed
- 150 km/h (93 mph).
- Range
- 200 km (124 miles)
- Propellers
- 2 pusher propellers, 8 VTOL-only propellers
- Electric motors
- 10 electric motors for the flight module
- Power source
- Battery packs (most likely)
- Cabin fuselage, flight module and ground chassis
- Carbon fiber composite
- Cabin module windows
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
- Flying module wings
- 1 main high wing with winglets
- Flying module tail
- Inverted U tail
- Ground module landing gear
- Intelligent ground chassis with 4 wheels
- 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.