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ARC Aerosystems · United Kingdom

C-600

ARC Aerosystems C-600

复合翼(升力+巡航) · 生产型设计 · 核查 2026-10-01

飞行构型与公司名称

复合翼(升力+巡航)

VFS 原始目录分组:升力+巡航。按目录所述推进方式归类。

核对构型依据 ↗

原始目录分组:升力+巡航

中文名称:待核实 · 原名:ARC Aerosystems

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。

资料覆盖与状态依据

可用性能指标 2/3 · 生产型设计 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗订阅本机型报道 RSS →

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.

明确提及本机型的报道

暂无明确匹配的公开报道;通用或重名型号不会自动关联。

目录参数变化记录

从保存的目录刷新快照比较,资料修改不等于实机性能发生变化。

暂无已保存的版本变化,后续目录刷新将保留快照。