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IO Aircraft · USA
QC-1
IO Aircraft QC-1
多旋翼 · 阶段未核实 · 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
- Cargo
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous or remote control
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 230 mph (370 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
- Hybrid-electric hydrogen turbine engine
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 4 propellers
- 续航时间
- 90 minutes
- 飞行高度
- 未公开／未录入
- 安全设计
- Has eight electric motors, if one or two electric motors fail, the other electric motors can handle landing the aircraft safely. There are multiple redundant avionics and electrical systems, the aircraft has a fireproof airframe and there is a whole aircraft ballistic parachute system. In case of an unexpected landing in water, the aircraft fuselage has been designed to float in water. There is a lithium battery backup providing five minutes for the aircraft providing time to land the aircraft safely. Once landed, the propeller nacelles fold against the sides of the fuselage for the safety on people on the ground.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL heavy-lift cargo drone
- Piloting
- Autonomous or remote control
- Capacity
- Cargo
- Cruise speed
- 230 mph (370 km/h)
- Flight time
- 90 minutes
- Range with payload
- More than 345 miles (556 km)
- Range without payload
- More than 1,151 miles (1,852 km)
- Maximum payload at 0-5,000 ft (0-1,524 m)
- 1,000 lb (454 kg)
- Maximum payload at 5,000-13,000 ft (1,524-3,962 m)
- 750 lb (340 kg)
- Propellers
- 4 propellers
- Electric Motors
- 8 electric motors
- Power source
- Hybrid-electric hydrogen turbine engine
- Fuselage
- Graphene composite
- Landing gear
- Unknown
- Water landings
- The aircraft can be outfitted with flotation devices for water landings.
- Safety features
- Has eight electric motors, if one or two electric motors fail, the other electric motors can handle landing the aircraft safely. There are multiple redundant avionics and electrical systems, the aircraft has a fireproof airframe and there is a whole aircraft ballistic parachute system. In case of an unexpected landing in water, the aircraft fuselage has been designed to float in water. There is a lithium battery backup providing five minutes for the aircraft providing time to land the aircraft safely. Once landed, the propeller nacelles fold against the sides of the fuselage for the safety on people on the ground.