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NASA Langley Research Center · USA
LA-8 eVTOL Testbed
NASA LA-8 eVTOL Testbed
矢量推力 · 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。
主要参数
- 座位／载员
- 未公开／未录入
- 乘客
- No passengers
- 驾驶方式
- Remote
- 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
- 65 lb (29.5 kg)
- 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
- 2 batteries. (Lithium polymer 8-cell (33.6 volts maximum) 22000 mAh batteries)
- 电机
- 8 electric motors. (Scorpion SII-4035 kV 450 electric motors)
- 旋翼／螺旋桨
- 8 propellers (Aeronaut CAM Carbon folding 16 inch x 8 inch pitch blades)
- 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.
全部原始参数
Specifications:
- Aircraft type
- eVTOL testbed
- Piloting
- Remote
- Passengers
- No passengers
- Cruise speed
- Unknown
- Maximum takeoff weight
- 65 lb (29.5 kg)
- Propellers
- 8 propellers (Aeronaut CAM Carbon folding 16 inch x 8 inch pitch blades)
- Electric Motors
- 8 electric motors. (Scorpion SII-4035 kV 450 electric motors)
- Power source
- 2 batteries. (Lithium polymer 8-cell (33.6 volts maximum) 22000 mAh batteries)
- Windows
- None
- Wings
- Tandem tiltwings including 4 elevons, 4 single-slotted Fowler flaps, 2 ruddervators (for a total of 20 independent control actuators)
- Fuselage (and wings)
- 3-D printed nylon and polycarbonate with some use of carbon fiber and aluminum for spars and internal fuselage walls.. 3D printing allows different configurations to be easily manufactured. The aircraft is also modular in design allowing different configurations to be assembled and tested. (80% of the aircraft is 3D printed)
- Tail
- 1 inverted V-tail
- Landing gear
- A tricycle type landing gear with one downward flange at the front of the aircraft and an inverted V-tail for its rear landing gear. A wheeled landing gear system has been designed for possible short takeoff and landing (STOL) testing.
- 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.