← eVTOL产品
SpyDar · USA
M-Star
SpyDar M-Star
升力＋巡航 · 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
- 2 medical personnel (Or 1 pilot and 1 doctor)
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous or piloted with automated assistance
- 航程（按来源口径）
- 63 miles (101 km)
- 巡航速度
- 150 mph (241 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 1,600 lb (725 kg)
- 载荷
- 400 lb (181 kg)
- 空重
- 1,200 lb (544 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
- 电机
- 36 electric motors
- 旋翼／螺旋桨
- 36 propellers
- 续航时间
- Unknown
- 飞行高度
- 3,000 ft (914 m)
- 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 in the sub-systems of the aircraft. The aircraft will have a ballistic parachute for emergency situations.
全部原始参数
Specifications:
- Aircraft type
- Autonomous eVTOL passenger aircraft
- Piloting
- Autonomous or piloted with automated assistance
- Capacity
- 2 medical personnel (Or 1 pilot and 1 doctor)
- Cruise speed
- 150 mph (241 km/h)
- Range
- 63 miles (101 km)
- Flight Time
- Unknown
- Cruise altitude
- 3,000 ft (914 m)
- Maximum payload
- 400 lb (181 kg)
- Empty weight
- 1,200 lb (544 kg)
- Maximum takeoff weight
- 1,600 lb (725 kg)
- Propellers
- 36 propellers
- Electric Motors
- 36 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Fuselage width
- 8.5 ft (2.6 m)
- Windows
- Panoramic wrap around bubble-type window allowing forward, left, right, top and bottom visibility for excellent views.
- Wings
- 1 low rear wing with winglets
- Landing gear
- Fixed quadricycle wheeled 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 in the sub-systems of the aircraft. The aircraft will have a ballistic parachute for emergency situations.