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Joby Aviation · USA
S4 2.0
Joby Aviation S4 2.0
矢量推力 · 原型机 · 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
- 4 passengers
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 150 miles (241.4 km)
- 巡航速度
- 未公开／未录入
- 最大速度
- 200 mph (322 km/h)
- 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
- 24 ft (7.3 m)
- 翼展
- 35 ft (10.7 m)
- 高度
- 未公开／未录入
- 动力来源
- 未公开／未录入
- 电机
- 6 high performance electric motors
- 旋翼／螺旋桨
- 6 tilt-prop, 4 propellers tilt vertically including the entire motor nacelle, 2 propellers tilt vertically with a linkage mechanism
- 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 of critical components in the sub-systems of the aircraft. The aircraft can also land like an airplane if necessary and has reserve battery power if there is an unexpected delayed when landing.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger air taxi pre-production prototype aircraft
- Pilot
- 1 pilot
- Passengers
- 4 passengers
- Maximum speed
- 200 mph (322 km/h)
- Range
- 150 miles (241.4 km)
- Propellers
- 6 tilt-prop, 4 propellers tilt vertically including the entire motor nacelle, 2 propellers tilt vertically with a linkage mechanism
- Motors
- 6 high performance electric motors
- Wingspan
- 35 ft (10.7 m)
- Length
- 24 ft (7.3 m)
- Weight
- 4,000 lb (1,815 kg)
- Windows
- Large windows for spectacular views for the passengers
- Fuselage
- Carbon fiber composite
- Wing
- 1 high main gull wing
- Tail
- 1 V tail
- Landing gear
- Tricycle wheeled retractable 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. The aircraft can also land like an airplane if necessary and has reserve battery power if there is an unexpected delayed when landing.