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Joby Aviation · USA

S4 1.0

Joby Aviation S4 1.0

矢量推力 · 技术验证机 · 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
未公开/未录入
乘客
0 people, no seats and no windows (The aircraft could hold 4 passengers if 4 seats were installed inside the aircraft)
驾驶方式
Remotely piloted
航程(按来源口径)
未公开/未录入
巡航速度
未公开/未录入
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
Batteries
电机
6 electric motors
旋翼/螺旋桨
6 tilt-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), if one of two motors stop working, the aircraft can make an emergency landing and land safely; redundancy of critical components; can land like an airplane if necessary; has reserve battery power if there is an unexpected delayed when landing

全部原始参数

Specifications:

Aircraft type
eVTOL full-scale technology demonstrator
Pilot
Remotely piloted
Passengers
0 people, no seats and no windows (The aircraft could hold 4 passengers if 4 seats were installed inside the aircraft)
Propellers
6 tilt-propellers
Motors
6 electric motors
Power source
Batteries
Fuselage
Composite
Windows
No windows
Tail
V-tail
Landing gear
Fixed tricycle wheeled landing gear
Safety features
Distributed Electric Propulsion (DEP), if one of two motors stop working, the aircraft can make an emergency landing and land safely; redundancy of critical components; can land like an airplane if necessary; has reserve battery power if there is an unexpected delayed when landing