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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。

资料覆盖与状态依据

可用性能指标 2/3 · 技术验证机 · 目录依据 · 目录阶段,尚未核实批准状态

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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.

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。