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ERC System GmbH · Germany
Charlie
ERC System Charlie
升力+巡航 · 概念设计 · 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
- 1 doctor, 1 patient and medical equipment The aircraft can hold two patients if there is less medical equipment on board.
- 乘客
- 未公开/未录入
- 驾驶方式
- 1 pilot
- 航程(按来源口径)
- 190 km (118 m)
- 巡航速度
- 200 km/h (124 mph)
- 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 (will be located in the wings)
- 电机
- 10 electric motors
- 旋翼/螺旋桨
- 10 propellers (8 VTOL-only propellers on two booms and 2 tractor propellers, for forward flight)
- 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) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.
全部原始参数
Specifications:
- Aircraft type
- Emergency medical services (EMS) passenger eVTOL aircraft (concept design)
- Piloting
- 1 pilot
- Capacity
- 1 doctor, 1 patient and medical equipment The aircraft can hold two patients if there is less medical equipment on board.
- Cruise speed
- 200 km/h (124 mph)
- Range
- 190 km (118 m)
- Maximum payload weight
- 450 kg (990 lb)
- Propellers
- 10 propellers (8 VTOL-only propellers on two booms and 2 tractor propellers, for forward flight)
- Electric motors
- 10 electric motors
- Power source
- Batteries (will be located in the wings)
- Fuselage
- Carbon fiber composite, cabin volume of 5.2 cubic meters (184 cubic feet), the rear door will have dimensions of 1.4 meters by 1.4 meters (4 feet 7 inches)
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility for excellent views for the pilot with a solid roof above the passenger compartment
- Doors
- 2 doors for the cockpit and 1 rear door for the patient
- Wings
- 1 high main wing and 2 booms for propellers
- Tail
- 1 high boom tail
- Landing gear
- Tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.