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Dufour Aerospace · Switzerland
Aero2
Dufour Aerospace Aero2
矢量推力 · 阶段未核实 · 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
- Cargo only (front loading)
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous
- 航程（按来源口径）
- 未公开／未录入
- 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
- 208 kg (459 lb)
- 载荷
- 52 kg (114 lb)
- 空重
- 156 kg (345 lb)
- 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
- 电机
- 4 electric motors
- 旋翼／螺旋桨
- 4 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), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft. The drone can land as a conventional airplane in an emergency.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL air cargo drone
- Piloting
- Autonomous
- Capacity
- Cargo only (front loading)
- Cruise speed
- 150 km/h (93 mph)
- Flight time and range
- 3 hour flight time with a 400 km (216 nm) range with a 40 kg (88 lb) payload
- Flight time and range
- 10.5 hour flight time with a 1,390 km (750 nm) range with a 10 kg (22 lb) payload
- Empty weight
- 156 kg (345 lb)
- Maximum payload
- 52 kg (114 lb)
- Maximum takeoff weight
- 208 kg (459 lb)
- Propellers
- 4 propellers
- Electric motors
- 4 electric motors
- Power source
- Hybrid-electric power source
- Fuselage
- Carbon fiber composite
- Wings
- 1 main high tilt-wing
- Tail
- 1 conventional tail with a downward vertical stabilizer
- Landing gear
- Fixed wheeled tail dragger configuration
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft. The drone can land as a conventional airplane in an emergency.