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Flyt Aerospace · USA

Mark III

Flyt Aerospace Mark III

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
There is a hypothetical cruise speed for the multicopter but because this is a prototype and is 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
802 lb (364 kg)
载荷
未公开/未录入
空重
444 lb (201 kg)
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
64 batteries
电机
4 electric motors
旋翼/螺旋桨
4 propellers
续航时间
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 defunct prototype multicopter aircraft
Piloting
1 pilot
Cruise speed
There is a hypothetical cruise speed for the multicopter but because this is a prototype and is 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
8 minutes
Empty weight
444 lb (201 kg)
Empty weight with batteries
552 lb (250 kg)
Maximum payload weight
250 lb (113 kg)
Maximum takeoff weight
802 lb (364 kg)
Propellers
4 propellers
Electric motors
4 electric motors
Power source
64 batteries
Fuselage
A vertical rectangular open-framed fuselage made from 4130 steel
Cockpit
Inside the middle of the open-framed fuselage
Landing gear
Fixed quadricycle 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.