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ELSA Industry · Romania
ELSA-H UAV
ELSA Industry ELSA-H UAV
矢量推力 · 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
- Cargo only
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote piloting and eventually autonomous piloting (Beyond Visual Line of Sight)
- 航程（按来源口径）
- 163-1,650 km (101-1,118 m), depending upon the power source
- 巡航速度
- 200 km/h (124 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 665 kg (1,466 lb)
- 载荷
- 未公开／未录入
- 空重
- 415 kg (915 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
- Batteries, hybrid-electric, hydrogen, kerosene-based, solar cells on aircraft)
- 电机
- 4 electric motors
- 旋翼／螺旋桨
- 4 propellers (front 2 propellers are tilt-propellers, rear 2 propellers are VTOL only)
- 续航时间
- 45 minutes - 7.3 hours Varies based on mission and power source (air cargo or surveillance )
- 飞行高度
- 未公开／未录入
- 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 passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.
全部原始参数
Specifications:
- Aircraft type
- eVTOL or hybrid-electric VTOL air cargo drone concept design
- Piloting
- Remote piloting and eventually autonomous piloting (Beyond Visual Line of Sight)
- Capacity
- Cargo only
- Cruise speed
- 200 km/h (124 mph)
- Range
- 163-1,650 km (101-1,118 m), depending upon the power source
- Flight time
- 45 minutes - 7.3 hours Varies based on mission and power source (air cargo or surveillance )
- Maximum cruise altitude
- 1,000-5,000 m (3,281-16,404 ft), depending upon the power source
- Empty weight
- 415 kg (915 lb)
- Maximum payload weight
- 250 kg (551 lb)
- Maximum takeoff weight
- 665 kg (1,466 lb)
- Propellers
- 4 propellers (front 2 propellers are tilt-propellers, rear 2 propellers are VTOL only)
- Electric motors
- 4 electric motors
- Power source
- Batteries, hybrid-electric, hydrogen, kerosene-based, solar cells on aircraft)
- Fuselage
- Carbon fiber composite
- Wings
- 1 main wing (can fold up during storage or transportation) with two booms
- Tail
- 1 boom tail with vertical stabilizers
- Landing gear
- Fixed quadricycle wheeled landing gear
- 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 passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.