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Land Rotor · USA
AAM Sportster
Land Rotor AAM Sportster
多旋翼 · 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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 30 miles (38 km) (the range can decrease or increase depending upon the power source, the wind conditions and weight of the pilot)
- 巡航速度
- 未公开／未录入
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 449 lb (204 kg)
- 载荷
- 200 lb (91 kg)
- 空重
- 249 lb (113 kg)
- 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, hydrogen and/or hybrid-electric biofuel
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers
- 续航时间
- 未公开／未录入
- 飞行高度
- Low altitude (road) flying
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft. There is also a redundant power supply. The aircraft is capable of having an emergency ballistic parachute installed on the aircraft.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger prototype aircraft
- Piloting
- 1 pilot
- Maximum cruise speed
- 50 mph (80 km/h)
- Range
- 30 miles (38 km) (the range can decrease or increase depending upon the power source, the wind conditions and weight of the pilot)
- Cruise altitude
- Low altitude (road) flying
- Empty weight
- 249 lb (113 kg)
- Maximum payload
- 200 lb (91 kg)
- Maximum takeoff weight
- 449 lb (204 kg)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Batteries, hydrogen and/or hybrid-electric biofuel
- Propeller length
- 22 inches (55.88 cm)
- Fuselage
- Carbon fiber composite, aircraft aluminum frame and landing skids
- Window
- Open cockpit
- Landing gear
- Fixed skid landing gear
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft. There is also a redundant power supply. The aircraft is capable of having an emergency ballistic parachute installed on the aircraft.