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Vehicle Systems, Dynamics and Design Laboratory · USA
LPC-01 Pushpak
Auburn University LPC-01 Pushpak
升力＋巡航 · 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
- 3 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- Two back-to-back 50 mile (80 km) trips (with a 20% battery power reserve)
- 巡航速度
- 201 mph (323 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 4,579 lb (2,077 kg)
- 载荷
- 未公开／未录入
- 空重
- 3,785 lb (1,717 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
- 旋翼／螺旋桨
- 10 propellers. 8 VTOL-only propellers and 2 cruise propellers for forward flight.
- 续航时间
- 未公开／未录入
- 飞行高度
- 3,000 ft (914.4 m)
- 安全设计
- Distributed electric propulsion (DEP) means having multiple propulsors (propellers + drive motors) so that if one or more propulsors fail, the other working propulsors 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. The lift-plus-cruise aircraft has no tilting components when transitioning between vertical and forward flight which increases safety by reducing complexity. The tricycle gear also allow the aircraft to land conventionally on a runway or road in emergencies.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers
- Cruise speed
- 201 mph (323 km/h)
- Range
- Two back-to-back 50 mile (80 km) trips (with a 20% battery power reserve)
- Cruise altitude
- 3,000 ft (914.4 m)
- Empty weight
- 3,785 lb (1,717 kg)
- Maximum payload weight
- 794 lb (360 kg)
- Maximum takeoff weight
- 4,579 lb (2,077 kg)
- Propellers
- 10 propellers. 8 VTOL-only propellers and 2 cruise propellers for forward flight.
- Electric motors
- 10 electric motors
- Power source
- Batteries
- Fuselage
- Material unknown
- Wing
- 1 high main wing, 39 ft (11.9 m) span
- Tail
- 2 downward boom mounted vertical stabilizers, one horizontal stabilizer
- Windows
- Larger side windows than a general aviation airplane
- Landing gear
- Fixed tricycle wheeled landing gear.
- Safety features
- Distributed electric propulsion (DEP) means having multiple propulsors (propellers + drive motors) so that if one or more propulsors fail, the other working propulsors 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. The lift-plus-cruise aircraft has no tilting components when transitioning between vertical and forward flight which increases safety by reducing complexity. The tricycle gear also allow the aircraft to land conventionally on a runway or road in emergencies.