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Pivotal · USA
Helix
Pivotal Helix
个人飞行器 · 生产型设计 · 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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 20+ miles (32+ km)
- 巡航速度
- 63 mph (101 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 568 lb (258 kg)
- 载荷
- 未公开／未录入
- 空重
- 348 lb (158 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
- Battery packs (8 kWh total storage)
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers
- 续航时间
- 未公开／未录入
- 飞行高度
- 未公开／未录入
- 安全设计
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
全部原始参数
Specifications:
- Aircraft type
- One passenger eVTOL production model aircraft
- Piloting
- 1 pilot
- Cruise speed
- 63 mph (101 km/h)
- Range
- 20+ miles (32+ km)
- Maximum climb and descent rate
- 500 fpm (152 mpm)
- Empty weight
- 348 lb (158 kg)
- Maximum payload weight
- 220 lb (100 kg)
- Maximum takeoff weight
- 568 lb (258 kg)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Battery packs (8 kWh total storage)
- Charging time
- Level 1 charger: 4.5 hours, Level 2 charger: 75 minutes
- Noise during cruise
- 72 dBa at 150 ft (46 m)
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wings
- Tandem wings
- Landing gear
- Fixed strut landing gear
- Safety features
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.