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ARC Aerosystems · United Kingdom
C-600
ARC Aerosystems C-600
升力＋巡航 · 生产型设计 · 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
- Cargo
- 乘客
- 未公开／未录入
- 驾驶方式
- Remotely (and in the future, autonomous)
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 120 km/h (74.5 mph)
- 最大速度
- 150 km/h (93 mph)
- 最大起飞重量
- 600 kg (1,322 lb)
- 载荷
- 150 kg (330 lb)
- 空重
- 340 kg (749 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
- Batteries
- 电机
- 9 electric motors
- 旋翼／螺旋桨
- 9 propellers (8 VTOL propellers, 1 pusher propeller)
- 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 in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- eVTOL and hybrid-electric VTOL cargo aircraft
- Piloting
- Remotely (and in the future, autonomous)
- Capacity
- Cargo
- Cruise speed
- 120 km/h (74.5 mph)
- Maximum speed
- 150 km/h (93 mph)
- Range (all-electric)
- 217 km (135 miles)
- Flight time (all-electric)
- 1 hour, 40 minutes
- Range (hybrid-electric)
- 644 km (400 miles)
- Flight time (hybrid-electric)
- 6 hours, 40 minutes
- Service ceiling
- 3,048 m (10,000 ft)
- Empty weight
- 340 kg (749 lb)
- Maximum payload
- 150 kg (330 lb)
- Maximum takeoff weight
- 600 kg (1,322 lb)
- Propellers
- 9 propellers (8 VTOL propellers, 1 pusher propeller)
- Electric motors
- 9 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Wings
- 1 main wing
- Tail
- T-tail
- Landing gear
- Fixed skid 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 in the sub-systems of the aircraft.