Zeva Aero (now Alpine Vertical) · USA

Zero

Zeva Aero (now Alpine Vertical) Zero

其他推力转向（待细分） · 原型机 · 核查 2026-10-01

飞行构型与公司名称

其他推力转向（待细分）

VFS 原始目录分组：矢量推力。尚无足够资料确定具体布局。

原始目录分组：矢量推力

中文名称：待核实 · 原名：Zeva Aero (now Alpine Vertical)

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。

可用性能指标 3/3 · 原型机 · 目录依据 · 目录阶段，尚未核实批准状态

座位／载员: 未公开／未录入
乘客: 未公开／未录入
驾驶方式: 1 pilot (Manually or remotely piloted)
航程（按来源口径）: 50 miles (80 km)
巡航速度: 160 mph (258 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: 220 lb (100 kg)
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: 8 electric motors
旋翼／螺旋桨: 8 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 in the sub-systems of the aircraft.

Aircraft type: Passenger eVTOL prototype aircraft aircraft
Piloting: 1 pilot (Manually or remotely piloted)
Cruise speed: 160 mph (258 km/h)
Range: 50 miles (80 km)
Maximum payload: 220 lb (100 kg)
Propellers: 8 propellers
Electric motors: 8 electric motors
Power source: Batteries
Fuselage: Carbon fiber composite and other material
Window: Canopy over cockpit
Landing gear: Retractable landing gear. The aircraft can dock vertically, to a side of a building.
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.

暂无明确匹配的公开报道；通用或重名型号不会自动关联。

从保存的目录刷新快照比较，资料修改不等于实机性能发生变化。

暂无已保存的版本变化，后续目录刷新将保留快照。