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School of Mechanical Engineering · India

Mistral

SASTRA University Mistral

倾转旋翼 · 概念设计 · 核查 2026-10-01

飞行构型与公司名称

倾转旋翼

Propellers: 6 tilt-propellers

核对构型依据 ↗

原始目录分组:矢量推力

中文名称:待核实 · 原名:School of Mechanical Engineering

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。

资料覆盖与状态依据

可用性能指标 3/3 · 概念设计 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗

概念参数,尚不代表已实现性能

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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.

明确提及本机型的报道

暂无明确匹配的公开报道;通用或重名型号不会自动关联。

目录参数变化记录

从保存的目录刷新快照比较,资料修改不等于实机性能发生变化。

暂无已保存的版本变化,后续目录刷新将保留快照。