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Ascendance Flight Technologies · France
ATEA
Ascendance Flight Technologies ATEA
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
- 5 seats (4 passengers and 1 pilot)
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 400 km (249 miles)
- 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
- 2,000 kilograms (4,410 pounds)
- 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
- Hybrid-electric. The hybrid engines are developed by the company. Batteries are used for VTOL flight and are charged during forward flight with the turbine engine.
- 电机
- 未公开／未录入
- 旋翼／螺旋桨
- 10 propellers. 8 dedicated VTOL propellers. 2 dedicated forward flight propellers and can reverse if needed during VTOL flight. (1 propeller for forward flight is on the nose and 1 propeller for forward flight is located on the tail of the aircraft.)
- 续航时间
- 未公开／未录入
- 飞行高度
- 未公开／未录入
- 安全设计
- 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. The aircraft has redundant electric propulsion, flight controls and can land conventionally on a runway if VTOL system isn't working.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL aircraft
- Piloting
- 1 pilot
- Capacity
- 5 seats (4 passengers and 1 pilot)
- Cruise speed
- 200 km/h (124 mph)
- Range
- 400 km (249 miles)
- Maximum flight time
- 2 hours
- Turn around time on ground
- 10 minutes
- Maximum take-off weight
- 2,000 kilograms (4,410 pounds)
- Propellers
- 10 propellers. 8 dedicated VTOL propellers. 2 dedicated forward flight propellers and can reverse if needed during VTOL flight. (1 propeller for forward flight is on the nose and 1 propeller for forward flight is located on the tail of the aircraft.)
- Power source
- Hybrid-electric. The hybrid engines are developed by the company. Batteries are used for VTOL flight and are charged during forward flight with the turbine engine.
- Emissions
- Emissions are reduced by 80%, according to the company
- Noise
- Noise pollution is 4 times less than a helicopter
- Wing configuration
- Canard wings
- Tail
- T-tail
- Landing gear
- Fixed tricycle wheeled landing gear
- Safety features
- 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. The aircraft has redundant electric propulsion, flight controls and can land conventionally on a runway if VTOL system isn't working.