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Korea Aerospace Research Institute (KARI) · South Korea
OPPAV
Korea Aerospace Research Institute (KARI) Optionally Piloted Personal Air Vehicle (OPPAV)
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
- 4-5 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- Pilot, remote or autonomous piloting
- 航程（按来源口径）
- 50 km (31 m)
- 巡航速度
- 200 km/h (124 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 500 kg (1,102 lb)
- 载荷
- 未公开／未录入
- 空重
- 未公开／未录入
- 长度
- 430 cm (14.1 ft)
- 翼展
- 未公开／未录入
- 高度
- 未公开／未录入
- 动力来源
- Lithium-ion battery packs
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 tilt-propellers (4 propellers are tilt-propellers and 4 propellers tilt with a tilting wing)
- 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 of critical components in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL scalable concept design aircraft
- Piloting
- Pilot, remote or autonomous piloting
- Capacity
- 4-5 passengers
- Cruise speed
- 200 km/h (124 mph)
- Range
- 50 km (31 m)
- Maximum takeoff weight
- 500 kg (1,102 lb)
- Propellers
- 8 tilt-propellers (4 propellers are tilt-propellers and 4 propellers tilt with a tilting wing)
- Electric motors
- 8 electric motors
- Power source
- Lithium-ion battery packs
- Fuselage
- Carbon fiber composite
- Length
- 430 cm (14.1 ft)
- Windows
- Panoramic wrap around windows allowing forward, left, right and top visibility for spectacular views
- Wings
- Canard wings
- Tail
- V tail
- 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 of critical components in the sub-systems of the aircraft.