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MEVA Aerospace sp z o.o. · Poland
MEVA X-1
MEVA Aerospace MEVA X-1
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 passenger
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- >100 km (>60 m)
- 巡航速度
- 未公开／未录入
- 最大速度
- 250 km/h (155 mph)
- 最大起飞重量
- 1,400 kg (3,086 lb)
- 载荷
- 未公开／未录入
- 空重
- Unknown
- 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
- Molicel battery packs
- 电机
- 10 electric motors (REB 60)
- 旋翼／螺旋桨
- 8 propellers (E-props) and are stacked propellers, 2 electric ducted fans (EDFs) (VF-570
- 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. The gull wing and inverted V-tail do have flaps or ailerons or both.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 1 passenger
- Maximum speed
- 250 km/h (155 mph)
- Range
- >100 km (>60 m)
- Empty weight
- Unknown
- Maximum takeoff weight
- 1,400 kg (3,086 lb)
- Propellers
- 8 propellers (E-props) and are stacked propellers, 2 electric ducted fans (EDFs) (VF-570
- Electric motors
- 10 electric motors (REB 60)
- Power source
- Molicel battery packs
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left, right an top visibility for spectacular views. (The windows could also qualify as a canopy over the cockpit window.)
- Doors
- 2 scissor doors (or swing-up doors)
- Wings
- 1 high main gull wing with winglets
- Tail
- 1 inverted V-tail
- Landing gear
- Fixed 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. The gull wing and inverted V-tail do have flaps or ailerons or both.