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LIFT Aircraft Inc. · USA

HEXA

LIFT Aircraft HEXA

多旋翼 · 阶段未核实 · 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。

资料覆盖与状态依据

可用性能指标 1/3 · 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
1 person
乘客
未公开/未录入
驾驶方式
The passenger can manually fly the aircraft, use voice commands or it can be flown by remote control
航程(按来源口径)
未公开/未录入
巡航速度
45 mph (72 km/h)
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
432 lb (196 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
Batteries
电机
18 electric motors
旋翼/螺旋桨
18 propellers
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 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. Has an autonomous ballistic parachute in case of a multiple rotor failure.

全部原始参数

Specifications:

Aircraft type
eVTOL multicopter amphibious passenger aircraft
Piloting
The passenger can manually fly the aircraft, use voice commands or it can be flown by remote control
Capacity
1 person
Cruise speed
45 mph (72 km/h)
Maximum cruise speed
63 mph (55 knots)
Maximum flying time
15 minutes
Empty weight
432 lb (196 kg)
Payload weight
250 lb (113 kg)
Propellers
18 propellers
Electric Motors
18 electric motors
Power source
Batteries
Fuselage
Carbon fiber composite
Windows
Front wind screen with open sides
Landing gear
The aircraft is amphibious and is capable of landing on both land and water. There are 4 perimeter floats for buoyancy and stability. The 5th center float is filled with energy-absorbing foam for added buoyancy and hard landing protection.
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. Has an autonomous ballistic parachute in case of a multiple rotor failure.

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。