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University of Maryland · USA
Starling
University of Maryland Starling
矢量推力 · 概念设计 · 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
- 4 passengers without mobility issues, 2 passengers with reduced mobility
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 109 m (175 km)
- 巡航速度
- 174 mph (278 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 5,553 lb (2,519 kg)
- 载荷
- 1,300 lb (590 kg)
- 空重
- 4,253 lb (1,929 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
- 12 electric motors
- 旋翼／螺旋桨
- 4 tilt-rotors
- 续航时间
- 50 minutes
- 飞行高度
- 4,000 ft (1,219.2 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. In case of total rotor failure, the aircraft can land like an airplane.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger concept design air taxi
- Piloting
- 1 pilot
- Capacity
- 4 passengers without mobility issues, 2 passengers with reduced mobility
- Cruise speed
- 174 mph (278 km/h)
- Range
- 109 m (175 km)
- Flight time
- 50 minutes
- Cruise altitude
- 4,000 ft (1,219.2 m)
- Empty weight
- 4,253 lb (1,929 kg)
- Maximum payload
- 1,300 lb (590 kg)
- Maximum takeoff weight
- 5,553 lb (2,519 kg)
- Propellers
- 4 tilt-rotors
- Electric motors
- 12 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Large windows allowing forward, left, right visibility, for spectacular views with a solid roof above the passenger compartment
- Wings
- Tandem wings
- 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 total rotor failure, the aircraft can land like an airplane.