Micor Technologies LLC · USA

Advanced Individual VTOL Aircraft (AIVA)

Micor Technologies Advanced Individual VTOL Aircraft (AIVA)

其他推力转向（待细分） · 阶段未核实 · 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：Micor Technologies LLC

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 · 阶段未核实 · 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 person
航程（按来源口径）: 87 km (hybrid-electric version has a long range)
巡航速度: 130 km/h (81 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: 110 kg (243 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: Batteries or hybrid-electric power source
电机: 10 or more
旋翼／螺旋桨: 10
续航时间: 未公开／未录入
飞行高度: 305 m (1,000 ft)
安全设计: Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft.

Aircraft type: eVTOL or hybrid-electric VTOL aircraft
Piloting: 1 person
Cruise speed: 130 km/h (81 mph)
Estimated maximum speed: 200 km/h (124 mph)
Range: 87 km (hybrid-electric version has a long range)
Cruise altitude: 305 m (1,000 ft)
Maximum payload: 110 kg (243 lb)
Battery reserve: 10 minutes
Propellers: 10
Electric Motors: 10 or more
Power source: Batteries or hybrid-electric power source
Cockpit: Open cockpit, motorcycle style
Fuselage: Carbon fiber
Landing gear: Unknown
Safety Features: Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land 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。