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Velo X Aerospace · USA
Velocitor X-1
Velo X Aerospace Velocitor X-1
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
- 1 person
- 乘客
- 未公开／未录入
- 驾驶方式
- Manual piloting with an auto take-off and landing capability
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 70 mph (113 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 760 lb (345 kg)
- 载荷
- 未公开／未录入
- 空重
- 500 lb (227 kg)
- 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
- Batteries
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers
- 续航时间
- 45 minutes (with a 15 minute reserve)
- 飞行高度
- 未公开／未录入
- 安全设计
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to enhance safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has a LIDAR obstacle warning and avoidance system (LOWAS) for safe avoidance of obstacles such as power lines, trees and structures. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity. There is a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL multicopter (concept design)
- Piloting
- Manual piloting with an auto take-off and landing capability
- Capacity
- 1 person
- Cruise speed
- 70 mph (113 km/h)
- Range (estimated)
- 60 m (97 km). The range of the multicopter depends upon the speed of the aircraft, weather conditions, altitude and other factors.
- Flight time
- 45 minutes (with a 15 minute reserve)
- Empty weight
- 500 lb (227 kg)
- Maximum payload weight
- 260 lb (118 kg)
- Maximum takeoff weight
- 760 lb (345 kg)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Cockpit
- Has front and rear windows with no doors. Uses an ultra-strong composite seat and a 4-point harness to provide a high level of safety and security.
- Windows
- Front and rear windshield with open sides
- Landing gear
- Fixed skid landing gear
- Safety features
- Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to enhance safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has a LIDAR obstacle warning and avoidance system (LOWAS) for safe avoidance of obstacles such as power lines, trees and structures. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity. There is a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.