跳到正文
← eVTOL产品

Vira Drones · Switzerland

M-750 Logistic

Vira Drones M-750 Logistic

多旋翼 · 概念设计 · 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
Air cargo only
乘客
未公开/未录入
驾驶方式
Autopilot or has remote controlled option
航程(按来源口径)
320 km (199 m)
巡航速度
125-150 km/h (77-92 mph)
最大速度
未公开/未录入
最大起飞重量
1,689 kg (3,724 lb)
载荷
未公开/未录入
空重
939 kg (2,070 lb)
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
Hybrid-electric power source
电机
6 electric motors
旋翼/螺旋桨
6 propellers
续航时间
未公开/未录入
飞行高度
3,000 m (9,843 ft)
安全设计
Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure.

全部原始参数

Specifications:

Aircraft type
Heavy-lift hybrid-electric VTOL concept design aircraft
Piloting
Autopilot or has remote controlled option
Capacity
Air cargo only
Cruise speed
125-150 km/h (77-92 mph)
Range
320 km (199 m)
Maximum altitude
3,000 m (9,843 ft)
Empty weight
939 kg (2,070 lb)
Maximum payload weight
750 kg (1,654 lb)
Maximum takeoff weight
1,689 kg (3,724 lb)
Propellers
6 propellers
Electric motors
6 electric motors
Power source
Hybrid-electric power source
Fuselage
Carbon fiber composite fuselage
Operating temperature range
-40 C (-40 F) to +50 C (122 F)
Landing gear
Lands on the bottom of the drone's fuselage (there are no landing skids, struts or wheels)
Safety features
Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure.