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Ascendance Flight Technologies · France
ATEA
Ascendance Flight Technologies ATEA
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 pilot, 3 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot, autonomous projected after 2030
- 航程（按来源口径）
- 450 km (280 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
- 未公开／未录入
- 载荷
- 450 kg (992 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
- 未公开／未录入
- 电机
- 未公开／未录入
- 旋翼／螺旋桨
- 未公开／未录入
- 续航时间
- 未公开／未录入
- 飞行高度
- 未公开／未录入
- 安全设计
- 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 airplane
- Pilot
- 1 pilot, autonomous projected after 2030
- Capacity
- 1 pilot, 3 passengers
- Cruise speed
- 200 km/h (124 mph)
- Range
- 450 km (280 miles)
- Payload
- 450 kg (992 lb)
- Gross weight
- 2,000 kg (4,400 lb)
- Turn around time on ground
- 10 minutes
- Propulsion for forward flight
- 1 nose-mounted propeller using a turbine engine for forward flight
- Propulsion for VTOL flight
- 3 lift fans powered by 3 electric motors using battery packs for low-noise take-off and landing. The VTOL fans are located in wings and forward fuselage.
- Batteries
- Used for VTOL and charged during forward flight with the turbine engine
- Wing configuration
- High main wing
- Tail
- Fuselage mounted vertical and horizontal stabilizers
- Landing gear
- Fixed tricycle wheeled landing gear
- Safety features
- Redundant electric propulsion, flight controls and can land conventionally on a runway if VTOL system isn't working