← eVTOL产品
School of Mechanical Engineering · India
Mistral
SASTRA University Mistral
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
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 500 km (311 miles)
- 巡航速度
- 200-250 km/h (124-155 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 1,255 kg (2,767 lb)
- 载荷
- 500 kg (1,102 lb)
- 空重
- 1,755 kg (3,869 lb)
- 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
- Battery packs (placed inside the wing with vents allowing the batteries to be cooled during flight)
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 tilt-propellers
- 续航时间
- Unknown
- 飞行高度
- 2,000 m (6,562 ft)
- 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 and the aircraft looses all power, the aircraft can glide and land on a runway or roadway.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger and air cargo aircraft
- Piloting
- 1 pilot
- Capacity
- 4 passengers
- Cruise speed
- 200-250 km/h (124-155 mph)
- Range
- 500 km (311 miles)
- Flight time
- Unknown
- Cruise altitude
- 2,000 m (6,562 ft)
- Empty weight
- 1,755 kg (3,869 lb)
- Maximum payload
- 500 kg (1,102 lb)
- Maximum takeoff weight
- 1,255 kg (2,767 lb)
- Propellers
- 6 tilt-propellers
- Electric motors
- 6 electric motors
- Power source
- Battery packs (placed inside the wing with vents allowing the batteries to be cooled during flight)
- Fuselage
- Aluminum
- Windows
- Panoramic wrap around windows allowing forward, left, right visibility, for spectacular views with a solid roof above the passenger compartment
- Wings
- 1 main high wing
- Tail
- V-tail
- 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 and the aircraft looses all power, the aircraft can glide and land on a runway or roadway.