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Aergility Corporation · USA
Atlis
Aergility Atlis Gen 3
升力＋巡航 · 原型机 · 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
- 40 cubic feet of cargo space with rear loading and unloading (96 in X 28 in X 26 in)
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous
- 航程（按来源口径）
- 300-600 miles (482-965 km)
- 巡航速度
- 100 mph (161 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 400-500 lb (181-227 kg)
- 空重
- 900 lb (408 kg)
- 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
- Multi-petroleum fuel and battery packs
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 1 propeller for forward flight, 6 rotors for VTOL flight.
- 续航时间
- 4.5 hours (with optional auxiliary tank)
- 飞行高度
- 未公开／未录入
- 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. When the cargo is outside of allowable center of gravity parameters, the aircraft will not take off. There are also redundancies in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- eVTOL heavy-lift autonomous cargo drone
- Piloting
- Autonomous
- Capacity
- 40 cubic feet of cargo space with rear loading and unloading (96 in X 28 in X 26 in)
- Cruise speed
- 100 mph (161 km/h)
- Range
- 300-600 miles (482-965 km)
- Flight time
- 4.5 hours (with optional auxiliary tank)
- Empty weight
- 900 lb (408 kg)
- Maximum payload
- 400-500 lb (181-227 kg)
- Propellers
- 1 propeller for forward flight, 6 rotors for VTOL flight.
- Turbo-engine
- 1 turboprop 90 kW multi-fuel engine
- Electric Motors
- 6 electric motors
- Power source
- Multi-petroleum fuel and battery packs
- Fuselage
- 3D printed composite fuselage
- Fuselage length
- 15.3 ft (4.66 m)
- Wings
- 1 main high-wing (3D printed)
- Tail
- 1 conventional tail
- Landing gear
- Fixed skid type 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. When the cargo is outside of allowable center of gravity parameters, the aircraft will not take off. There are also redundancies in the sub-systems of the aircraft.