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University of Maryland · USA
Blitzen
University of Maryland Blitzen
电动旋翼机 · 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 passenger, 2 passengers with disabilities
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- Over 100 m (161 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
- 5,717 lb (2,593 kg)
- 载荷
- 1,232 lb (559 kg)
- 空重
- 4,485 lb (2,034 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 (6 electric motors for the main rotorblade, 4 electric motors for the tailrotor)
- 旋翼／螺旋桨
- 未公开／未录入
- 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 (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 helicopter can autorotate in case all electric motors fail.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger helicopter
- Piloting
- 1 pilot
- Capacity
- 4 passenger, 2 passengers with disabilities
- Cruise speed
- 150 mph (241 km/h)
- Range
- Over 100 m (161 km)
- Empty weight
- 4,485 lb (2,034 kg)
- Maximum payload
- 1,232 lb (559 kg)
- Maximum takeoff weight
- 5,717 lb (2,593 kg)
- Rotorblade
- 1 main rotorblade
- Tail propeller
- 1 pusher tail propeller
- Electric motors
- 10 electric motors (6 electric motors for the main rotorblade, 4 electric motors for the tailrotor)
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Large helicopter type windows
- Wings
- 1 high main wing
- Tail
- 1 rear standard helicopter tail with with rear horizontal stabilizers
- 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 in the sub-systems of the aircraft. The helicopter can autorotate in case all electric motors fail.