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Vira Drones · Switzerland
M-500 Logistic
Vira Drones M-500 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
- 1,125 kg (2,480 lb)
- 载荷
- 未公开／未录入
- 空重
- 625 kg (1,378 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
- 4 electric motors
- 旋翼／螺旋桨
- 4 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
- 625 kg (1,378 lb)
- Maximum payload weight
- 500 kg (1,102 lb)
- Maximum takeoff weight
- 1,125 kg (2,480 lb)
- Propellers
- 4 propellers
- Electric motors
- 4 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.