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Katla Aero AB · Sweden
Katla 700
Katla Aero Katla 700
升力＋巡航 · 阶段未核实 · 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
- 2 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- Unknown
- 航程（按来源口径）
- 200 km (124 m)
- 巡航速度
- 未公开／未录入
- 最大速度
- 450 km/h (280 mph)
- 最大起飞重量
- 未公开／未录入
- 载荷
- 200 kg (441 lb)
- 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
- 12 electric motors
- 旋翼／螺旋桨
- 10 fixed VTOL propellers and 2 fixed forward flight propellers
- 续航时间
- Unknown
- 飞行高度
- Unknown
- 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 passenger and/or cargo aircraft
- Piloting
- Unknown
- Capacity
- 2 passengers
- Maximum speed
- 450 km/h (280 mph)
- Range
- 200 km (124 m)
- Flight Time
- Unknown
- Cruise altitude
- Unknown
- Maximum payload
- 200 kg (441 lb)
- Propellers
- 10 fixed VTOL propellers and 2 fixed forward flight propellers
- Electric Motors
- 12 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Canopy over cockpit allowing forward, left, right, top and rear visibility, for spectacular views for the passengers
- Wings
- Novel closed-wing design
- Tail
- V-tail which is seamlessly connected to the aircraft's closed-wing
- Landing gear
- Retractable 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 in the sub-systems of the aircraft.