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Flyt Aerospace · USA

FlytCycle 16

Flyt Aerospace FlytCycle 16

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
617 lb (280 kg)
载荷
300 lb (136 kg)
空重
189 lb (86 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
96 batteries
电机
16 electric motors
旋翼/螺旋桨
16 propellers
续航时间
10 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 passenger multicopter aircraft
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
10 minutes
Empty weight
189 lb (86 kg)
Empty weight with batteries
317 lb (144 kg)
Maximum payload
300 lb (136 kg)
Maximum takeoff weight
617 lb (280 kg)
Propellers
16 propellers
Electric motors
16 electric motors
Power source
96 batteries
Battery weight
128 lb (58 kg)
Fuselage
4130 steel
Window
Open cockpit
Landing gear
Fixed skid 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.