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Zapata · France

AirScooter

Zapata AirScooter

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
航程(按来源口径)
未公开/未录入
巡航速度
80 km/h (50 mph)
最大速度
100 km/h (62 mph)
最大起飞重量
232 kg (511 lb) +
载荷
120 kg (264 lb)
空重
112 kg (247 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
14 electric motors
旋翼/螺旋桨
14 propellers on 8 booms (4 booms have 2 propellers each and 2 of these booms have an additional vertical yaw control propellers. Each of these booms have a VTOL propeller at the end and under the booms and there is also another propeller that is located in the middle of the boom, under the boom. The other 4 booms have 4 propellers at the top and at the end of these booms.)
续航时间
2 hours +
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 of critical components in the sub-systems of the aircraft.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL passenger multicopter aircraft
Piloting
1 pilot
Cruise speed
80 km/h (50 mph)
Maximum speed
100 km/h (62 mph)
Flight time
2 hours +
Empty weight
112 kg (247 lb)
Maximum payload
120 kg (264 lb)
Maximum takeoff weight
232 kg (511 lb) +
Propellers
14 propellers on 8 booms (4 booms have 2 propellers each and 2 of these booms have an additional vertical yaw control propellers. Each of these booms have a VTOL propeller at the end and under the booms and there is also another propeller that is located in the middle of the boom, under the boom. The other 4 booms have 4 propellers at the top and at the end of these booms.)
Electric motors
14 electric motors
Power source
Hybrid-electric power source
Fuel tank
18.9 L (5 gallons)
Fuselage
Carbon fiber composite
Dimensions
340 X 340 X 256 (L X W X H, cm), 11 X 11 X 8 (feet)
Window
1 long, high window. (The concept design had 1 window on each side of the cockpit. The prototype does not have any windows on the side of the cockpit.)
Tail
1 horizontal stabilizer tail, very similar to a high boom tail
Landing gear
Fixed tricycle strut landing gear
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 of critical components in the sub-systems of the aircraft.