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Wisk Aero LLC. · USA
Generation 5, Cora
Wisk Aero Generation 5, Cora
升力+巡航 · 原型机 · 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
- 未公开/未录入
- 乘客
- 2 passengers
- 驾驶方式
- Autonomous
- 航程(按来源口径)
- 62 miles (100 km)
- 巡航速度
- 110 mph (180 km/h)
- 最大速度
- 未公开/未录入
- 最大起飞重量
- 未公开/未录入
- 载荷
- 400 lb (181 kg)
- 空重
- 未公开/未录入
- 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
- Electric power source
- 电机
- 未公开/未录入
- 旋翼/螺旋桨
- 12 VTOL-only propellers and 1 pusher propeller
- 续航时间
- 19 minutes with a 10 minute reserve
- 飞行高度
- 10,000 ft (3.04 km)
- 安全设计
- Distributed Electric Propulsion (DEP) allows multiple propellers for VTOL flight, if several of the propellers stop working for any reason, the aircraft can still land safely. Triple Redundant Flight-Computer, equipped with three independent flight-computers that each calculate its location. If there’s an issue with one of them, the aircraft can still reliably navigate. There is no single point of failure. The aircraft also has a parachute if all else fails.
全部原始参数
Specifications:
- Aircraft
- Autonomous passenger eVTOL aircraft (prototype)
- Piloting
- Autonomous
- Passengers
- 2 passengers
- Cruising speed
- 110 mph (180 km/h)
- Cruising altitude
- Operates between 500 ft to 3,000 ft (150 m to 900 m)
- Maximum altitude
- 10,000 ft (3.04 km)
- Range
- 62 miles (100 km)
- Flight time
- 19 minutes with a 10 minute reserve
- Payload
- 400 lb (181 kg)
- Propellers
- 12 VTOL-only propellers and 1 pusher propeller
- Power source
- Electric power source
- Main wing
- 1 low main wing with 2 flaps and winglets on each wing, 36 feet (11 m)
- Tail
- 1 twin boom tail with an inverted U horizontal stabilizer with 4 flaps
- Landing gear
- Fixed tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP) allows multiple propellers for VTOL flight, if several of the propellers stop working for any reason, the aircraft can still land safely. Triple Redundant Flight-Computer, equipped with three independent flight-computers that each calculate its location. If there’s an issue with one of them, the aircraft can still reliably navigate. There is no single point of failure. The aircraft also has a parachute if all else fails.