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Alpine Vertical · USA
Argon
Alpine Vertical (formerly Zeva Aero) Argon
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）
- 379 miles (609 km)
- 巡航速度
- 140 mph (224 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
- 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 and batteries
- 电机
- 5 electric motors
- 旋翼／螺旋桨
- 1 tractor propeller (for forward flight), 4 VTOL propellers
- 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), 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 of critical components in the sub-systems of the aircraft. The aircraft can land conventionally if VTOL propellers stop turning. An optional whole aircraft emergency ballistic parachute can be ordered for the aircraft. The aircraft is still flyable with a 100% loss of power.
全部原始参数
Specifications:
- Aircraft type
- Passenger long-range hybrid-electric VTOL (and CTOL optional) concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 1 passenger
- Cruise speed
- 140 mph (224 km/h)
- Range
- 379 miles (609 km)
- Useful load
- 650 lbs (294 kg)
- Propellers
- 1 tractor propeller (for forward flight), 4 VTOL propellers
- Electric motors
- 5 electric motors
- Power source
- Hybrid-electric and batteries
- Fuselage
- Carbon fiber composite
- Windows
- Typical general aviation aircraft windows
- Wings
- 1 main high wing
- Tail
- 1 T-tail
- Landing gear
- Fixed tricycle 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 of critical components in the sub-systems of the aircraft. The aircraft can land conventionally if VTOL propellers stop turning. An optional whole aircraft emergency ballistic parachute can be ordered for the aircraft. The aircraft is still flyable with a 100% loss of power.