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Maglev Aero · USA
HyperDrive Propulsion System
Maglev Aero
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。
核对构型依据 ↗原始目录分组：矢量推力
中文名称：待核实 · 原名：Maglev Aero
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。
资料覆盖与状态依据
可用性能指标 0/3 · 阶段未核实 · 目录依据 · 目录阶段，尚未核实批准状态
查看状态依据 ↗订阅本机型报道 RSS →主要参数
- 座位／载员
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 未公开／未录入
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 未公开／未录入
- 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
- Batteries
- 电机
- 未公开／未录入
- 旋翼／螺旋桨
- The HyperDrive system consists of many bladed annular rotors suspended, guided and rim-driven by a circular maglev system
- 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. If there is a loss in one ore more inverters, it will not reduce the number of blades providing lift and control. If there is a total power failure, the aircraft can autorotate and land.
全部原始参数
Specifications:
- Aircraft type
- eVTOL propulsion system
- Propellers
- The HyperDrive system consists of many bladed annular rotors suspended, guided and rim-driven by a circular maglev system
- Number of electric motors
- Unknown
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- 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. If there is a loss in one ore more inverters, it will not reduce the number of blades providing lift and control. If there is a total power failure, the aircraft can autorotate and land.
明确提及本机型的报道
暂无明确匹配的公开报道；通用或重名型号不会自动关联。
目录参数变化记录
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。