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Joby Aviation · USA
S4
Joby Aviation S4
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
- 4 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 100 miles (161 km), including energy reserves
- 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 high performance dual wound electric motors
- 旋翼／螺旋桨
- 6 tilt-prop, 4 propellers tilt vertically including the entire electric 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.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL aircraft
- Piloting
- 1 pilot
- Capacity
- 4 passengers
- Maximum cruise speed
- 200 mph (322 km/h)
- Range
- 100 miles (161 km), including energy reserves
- Empty weight (approximately)
- 4,300 lb (1,950 kg)
- Maximum payload (approximately)
- 1,000 lb (453 kg)
- Maximum takeoff weight (approximately)
- 5,300 lb (2,404 kg)
- Propellers
- 6 tilt-prop, 4 propellers tilt vertically including the entire electric motor nacelle, 2 propellers tilt vertically with a linkage mechanism
- Electric motors
- 6 high performance dual wound electric motors
- Power source
- Batteries
- Noise Footprint
- 45 dBA in cruise
- Peak Power
- 236 kW per electric motor
- Weight of Dual-Wound Motor Plus Inverter
- 28 kg
- Peak Torque
- 1,237 lb•ft (pound-feet) 1,800 N•m (newton-meters)
- Continuous Torque
- 1,027 lb•ft (1,380 N•m)
- Cell-Level Specific Energy
- 288 W•h/kg (watt-hour per kilogram)
- Flight Cycles
- 10,000 plus
- Pack-Level Specific Energy
- 235 W•h/kg
- Fuselage
- Carbon fiber composite
- Windows
- Large windows for the entire cabin for spectacular views for the passengers
- Wing
- 1 high main gull wing
- Tail
- 1 V tail
- Landing gear
- Tricycle wheeled 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.