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Vinata Aeromobility · India
Flying Car
Vinata Aeromobility Flying Car
多旋翼 · 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
- 2 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous AI cockpit
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 未公开／未录入
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 1,300 kg (2,866 lb)
- 载荷
- 未公开／未录入
- 空重
- 990 kg (2,183 lb)
- 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 Lithium-ion batteries
- 电机
- 12 electric motors (8 for propellers, 4 for ground wheels)
- 旋翼／螺旋桨
- 8 propellers
- 续航时间
- 60 minutes
- 飞行高度
- 914 m (3,000 ft)
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. There aircraft has a whole aircraft emergency ballistic parachute system and a return-to-home capability.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL aircraft and road vehicle
- Piloting
- Autonomous AI cockpit
- Capacity
- 2 passengers
- Cruise speed (air)
- 120 km/h (75 mph)
- Range (air)
- 100 km (62 miles)
- Flight time
- 60 minutes
- Maximum altitude
- 914 m (3,000 ft)
- Empty weight
- 990 kg (2,183 lb)
- Maximum payload weight
- 310 kg (683 lb)
- Maximum takeoff weight
- 1,300 kg (2,866 lb)
- Propellers
- 8 propellers
- Electric Motors
- 12 electric motors (8 for propellers, 4 for ground wheels)
- Power source
- Hybrid-electric power source with Lithium-ion batteries
- Fuselage
- Carbon fiber composite
- Doors
- Gull-wing doors
- Windows
- Larger windows allowing for forward, left, right and top views for the passengers
- Tail
- V-tail
- Landing gear
- 4 fixed quadricycle wheeled landing gear which are also used for road travel
- Safety Features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. There aircraft has a whole aircraft emergency ballistic parachute system and a return-to-home capability.