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Georgia Institute of Technology · USA
Balto
Georgia Institute of Technology Balto
升力＋巡航 · 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
- 4 passengers or a maximum of 2 passengers with reduced mobility and their caregivers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 156 m (252 km)
- 巡航速度
- 121 mph (194 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
- 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
- 10 electric motors
- 旋翼／螺旋桨
- 10 propellers
- 续航时间
- 49 minutes
- 飞行高度
- 45,900 ft (14,000 meters)
- 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. If there is a total propeller failure, the aircraft can like a regular airplane.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger aircraft
- Piloting
- 1 pilot
- Capacity
- 4 passengers or a maximum of 2 passengers with reduced mobility and their caregivers
- Cruise speed
- 121 mph (194 km/h)
- Range
- 156 m (252 km)
- Flight time
- 49 minutes
- Maximum altitude
- 45,900 ft (14,000 meters)
- Propellers
- 10 propellers
- Electric motors
- 10 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Larger than conventional windows allowing left, right and some forward visibility for spectacular views with a solid roof above the passenger compartment
- Window
- Canopy over cockpit
- Wings
- 1 main high wing with winglets
- Tail
- Conventional tail
- Landing gear
- Retractable 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. If there is a total propeller failure, the aircraft can like a regular airplane.