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UASystems SA · Switzerland
eZELOS S3 Twin-Hybrid Air Taxi
UASystems eZELOS S3 Twin-Hybrid Air Taxi
电动旋翼机 · 停研/历史型号 · 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 3/3 · 停研/历史型号 · 目录阶段,尚未核实批准状态
查看状态依据 ↗订阅本机型报道 RSS →主要参数
- 座位/载员
- 2 passengers
- 乘客
- 未公开/未录入
- 驾驶方式
- 1 pilot
- 航程(按来源口径)
- 500+ km (311 m)
- 巡航速度
- 280 km/h (174 mph)
- 最大速度
- 320 km/h (199 mph)
- 最大起飞重量
- 未公开/未录入
- 载荷
- 500+ kg (1,102 lb)
- 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, piston engines and batteries
- 电机
- 6 electric motors. If one or two of the electric motors for the main rotorblades fail, the other electric motors are built for redundancy and will help the helicopter land safely.
- 旋翼/螺旋桨
- 未公开/未录入
- 续航时间
- 未公开/未录入
- 飞行高度
- 未公开/未录入
- 安全设计
- In case of a power loss, the helicopter can land using autorotation. The company also has redundancy built into the aircraft providing an additional margin of safety.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric defunct concept design helicopter air taxi
- Piloting
- 1 pilot
- Capacity
- 2 passengers
- Cruise speed
- 280 km/h (174 mph)
- Maximum speed
- 320 km/h (199 mph)
- Range
- 500+ km (311 m)
- Maximum payload
- 500+ kg (1,102 lb)
- Rotorblades
- 2 coaxial rotorblades (4 blades per rotorblade)
- Pusher propellers
- 2 electric ducted fans (pusher ducted fans)
- Electric Motors
- 6 electric motors. If one or two of the electric motors for the main rotorblades fail, the other electric motors are built for redundancy and will help the helicopter land safely.
- Power source
- Hybrid-electric, piston engines and batteries
- Fuselage
- Carbon fiber composite
- Windows
- Standard helicopter windows
- Wings
- At the lower front of the fuselage, there are stub wings with small winglets
- Tail boom type
- The helicopter has no tail but there is a small downward facing vertical stabilizer protruding from the rear of the helicopter
- Landing gear
- Fixed skid landing gear
- Safety features
- In case of a power loss, the helicopter can land using autorotation. The company also has redundancy built into the aircraft providing an additional margin of safety.
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。