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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 · 技术验证机 · 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
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote control and has auto hover capability and auto landing capability
- 航程（按来源口径）
- 20 km (12 m)
- 巡航速度
- 110 km/h (68 mph)
- 最大速度
- 125 km/h (78 mph)
- 最大起飞重量
- 46 kg (101 lb)
- 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
- 3.1 m (10 feet, 1.7 in)
- 高度
- 未公开／未录入
- 动力来源
- Battery packs
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers (4 tilt-propellers, 4 VTOL-only propellers)
- 续航时间
- 30 minutes
- 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
- eVTOL 44% subscale technology demonstrator
- Piloting
- Remote control and has auto hover capability and auto landing capability
- Capacity
- No passengers
- Cruise speed
- 110 km/h (68 mph)
- Maximum speed
- 125 km/h (78 mph)
- Range
- 20 km (12 m)
- Flight time
- 30 minutes
- Maximum takeoff weight
- 46 kg (101 lb)
- Propellers
- 8 propellers (4 tilt-propellers, 4 VTOL-only propellers)
- Electric motors
- 8 electric motors
- Power source
- Battery packs
- Fuselage
- Carbon fiber composite
- Windows
- Painted on windows
- Wings
- 1 main high wing
- Wing span
- 3.1 m (10 feet, 1.7 in)
- Tail
- 1 conventional tail
- Landing gear
- Fixed 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 of critical components in the sub-systems of the aircraft.