← eVTOL产品
Harmony Aeronautics · USA
Harmony
Texas A&M University, Harmony Aeronautics, Harmony
个人飞行器 · 原型机 · 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
- Uncrewed
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote control
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- Unknown
- 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
- 未公开／未录入
- 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
- 2 electric motors
- 旋翼／螺旋桨
- 2 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) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. 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 for the Harmony subscale eVTOL multicopter:
- Aircraft type
- Uncrewed 1/3 subscale eVTOL multicopter aircraft (prototype)
- Piloting
- Remote control
- Capacity
- Uncrewed
- Cruise speed
- Unknown
- Empty weight (estimated)
- 184 lb (84 kg)
- Propellers
- 2 propellers
- Electric motors
- 2 electric motors
- Power source
- Batteries
- Cockpit
- Open cockpit
- Fuselage
- Unknown
- Landing gear
- Fixed skid landing gear
- Safety features
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. 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.
Specifications for the Harmony full-scale eVTOL multicopter:
- Aircraft type
- Uncrewed full-scale eVTOL multicopter aircraft (prototype)
- Piloting
- Remote control
- Capacity
- Cargo only
- Cruise speed
- Unknown
- Empty weight
- 550 lb (250 kg)
- Maximum payload weight
- 200 lb (91 kg)
- Maximum takeoff weight
- 750 lb (340 kg)
- Propellers
- 2 propellers
- Electric motors
- 2 electric motors
- Power source
- Batteries
- Fuselage
- Unknown
- Landing gear
- Fixed skid landing gear
- Safety features
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. 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.