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University of Illinois · USA
Illini Air Shuttle
University of Illinois Illini Air Shuttle
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
- 10 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- Unknown
- 航程（按来源口径）
- 200 miles (321 km)
- 巡航速度
- 180 mph (290 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 10,765 lb (4,882 kg)
- 载荷
- 2,756 lb (1,250 kg)
- 空重
- 8,009 lb (3,632 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
- 10 electric motors
- 旋翼／螺旋桨
- 10 propellers
- 续航时间
- 1 hour
- 飞行高度
- Unknown
- 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. In case of emergency, the aircraft can glide and land on a runway or road.
全部原始参数
Specifications:
- Aircraft type
- Medium size eVTOL passenger aircraft
- Piloting
- Unknown
- Capacity
- 10 passengers
- Cruise speed
- 180 mph (290 km/h)
- Range
- 200 miles (321 km)
- Flight time
- 1 hour
- Cruise altitude
- Unknown
- Empty weight
- 8,009 lb (3,632 kg)
- Maximum payload
- 2,756 lb (1,250 kg)
- Maximum takeoff weight
- 10,765 lb (4,882 kg)
- Propellers
- 10 propellers
- Electric motors
- 10 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Large windows allowing left, right visibility, for spectacular views with a solid roof above the passenger compartment
- Wings
- Tandem wings
- Tail
- No tail but appears to have a rear cargo loading ramp
- Landing gear
- Retractable tricycle 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. In case of emergency, the aircraft can glide and land on a runway or road.