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Vehicle Systems, Dynamics and Design Laboratory · USA
VT-02 Sevak
Auburn University VT-02 Sevak
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
- No passengers but the aircraft can be scaled for air taxi and air cargo service
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote controlled
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- Unknown
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 353 lb (160 kg)
- 载荷
- 未公开／未录入
- 空重
- 未公开／未录入
- 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
- Hybrid-electric power source with one turbine engine and batteries
- 电机
- 10 electric motors
- 旋翼／螺旋桨
- 10 propellers (6 propellers on a tilting spar, 2 VTOL propellers in the nose of the aircraft and 2 VTOL propeller in the tail of the aircraft)
- 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) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.
全部原始参数
Specifications:
- Aircraft type
- Passenger hybrid-electric VTOL scalable concept design aircraft
- Piloting
- Remote controlled
- Capacity
- No passengers but the aircraft can be scaled for air taxi and air cargo service
- Cruise speed
- Unknown
- Maximum takeoff weight
- 353 lb (160 kg)
- Propellers
- 10 propellers (6 propellers on a tilting spar, 2 VTOL propellers in the nose of the aircraft and 2 VTOL propeller in the tail of the aircraft)
- Electric motors
- 10 electric motors
- Power source
- Hybrid-electric power source with one turbine engine and batteries
- Fuselage
- Carbon fiber composite
- Wings
- 1 canard and 1 high main wing
- High main wing, wingspan
- 18.57 ft (5.66 m)
- Canard wing span
- 11.87 ft (3.62 m)
- Tail
- 1 vertical stabilizer
- Landing gear
- Retractable tricycle wheeled landing gear
- Safety features
- Distributed electric propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.