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Flyt Aerospace · USA

FlytCycle Hoverboard

Flyt Aerospace Hoverboard

多旋翼 · 停研/历史型号 · 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
未公开/未录入
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
未公开/未录入
巡航速度
While there is a hypothetical cruise speed for the multicopter it was never flown at the actual cruise speed because this is a prototype and was only flown close to the ground for testing purposes. The aircraft was never intended to be flown at what would be considered its cruise speed.
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
8 electric motors
旋翼/螺旋桨
8 propellers (no shielding around the propellers)
续航时间
6-8 minutes
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.

全部原始参数

Specifications:

Aircraft type
eVTOL one passenger multicopter hoverboard
Piloting
1 pilot
Cruise speed
While there is a hypothetical cruise speed for the multicopter it was never flown at the actual cruise speed because this is a prototype and was only flown close to the ground for testing purposes. The aircraft was never intended to be flown at what would be considered its cruise speed.
Flight time
6-8 minutes
Propellers
8 propellers (no shielding around the propellers)
Electric motors
8 electric motors
Power source
Batteries
Fuselage
4130 steel
Cockpit
Open cockpit, the pilot stands in secured shoes that are bolted to the top of the substructure
Landing gear
4 fixed landing struts
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.