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MACA Aviation & Aerospace · France
S11
MACA Aviation & Aerospace S11
多旋翼 · 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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot with semi-autonomous piloting
- 航程（按来源口径）
- Unknown
- 巡航速度
- 未公开／未录入
- 最大速度
- 250 km/h (155 mph)
- 最大起飞重量
- 未公开／未录入
- 载荷
- 未公开／未录入
- 空重
- 600 kg (1,322 lb)
- 长度
- 7 meters (~23 feet)
- 翼展
- 未公开／未录入
- 高度
- 未公开／未录入
- 动力来源
- Hybrid-electric (hydrogen fuel cells)
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 propellers
- 续航时间
- Unknown
- 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.
全部原始参数
Specifications:
- Aircraft type
- Racing hybrid-electric VTOL Formula 1 air racing aircraft
- Piloting
- 1 pilot with semi-autonomous piloting
- Maximum speed
- 250 km/h (155 mph)
- Range
- Unknown
- Flight Time
- Unknown
- Empty weight
- 600 kg (1,322 lb)
- Maximum payload weight (for the pilot)
- 79 kg (175 lb)
- Propellers
- 6 propellers
- Electric Motors
- 6 electric motors
- Power source
- Hybrid-electric (hydrogen fuel cells)
- Fuselage
- Carbon fiber composite
- Length
- 7 meters (~23 feet)
- Windows
- Canopy over cockpit
- Wings
- Front and rear canard-type wings with winglets
- Landing gear
- Lands on the bottom of the front and rear wings
- 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.