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Zero Gravity Aircraft Industry Co., LTD. · China
ZG-T6
Zero Gravity (ZeroG) ZG-T6
矢量推力 · 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
- 5 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot (in the future, it will be autonomous)
- 航程（按来源口径）
- 300 km (186 m)
- 巡航速度
- 250 km/h (155 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 2,500 kg (5,512 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
- 未公开／未录入
- 高度
- 未公开／未录入
- 动力来源
- Batteries
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 tilt-propellers
- 续航时间
- 90 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 in the sub-systems of the aircraft. In case all systems fail, the aircraft also has an emergency ballistic parachute to keep the passengers safe during an emergency landing.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger and air cargo concept design aircraft
- Piloting
- 1 pilot (in the future, it will be autonomous)
- Capacity
- 5 passengers
- Cruise speed
- 250 km/h (155 mph)
- Range
- 300 km (186 m)
- Flight Time
- 90 minutes
- Maximum takeoff weight
- 2,500 kg (5,512 lb)
- Propellers
- 6 tilt-propellers
- Electric Motors
- 6 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility, for spectacular views
- Wings
- 1 high main wing, 1 forewing
- Tail
- 1 V-tail (with a small inverted V at the base of the V 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 in the sub-systems of the aircraft. In case all systems fail, the aircraft also has an emergency ballistic parachute to keep the passengers safe during an emergency landing.