← eVTOL产品
Sukhoi Design Bureau · Russia
S-76 Atlas Transport
United Aircraft Corp Sukhoi S-76 Atlas Transport
升力＋巡航 · 原型机 · 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
- Air cargo. 2 cubic meters (2 m3), (71 ft.3) cargo hold. The aircraft can hold two standard 80 cm X 120 cm X 14.4 cm (2 ft, 7.5 in X 3 ft, 11.2 in X 5.75 in) pallets or two transport containers. The cargo is loaded at the front of the aircraft.
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous piloting
- 航程（按来源口径）
- 1,000 km (621 m)
- 巡航速度
- 180 km/h (112 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 1,500 kg (3,307 lb)
- 载荷
- 未公开／未录入
- 空重
- 1,200 kg (2,646 lb)
- 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
- Internal combustion engine and battery packs
- 电机
- 9 electric motors
- 旋翼／螺旋桨
- 9 propellers (8 VTOL propellers, 1 pusher propeller)
- 续航时间
- 未公开／未录入
- 飞行高度
- 4,000 m (13,123 ft)
- 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 passengers or cargo. 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 no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.
全部原始参数
Specifications:
- Aircraft type
- Long range heavy-lift uncrewed air cargo eVTOL drone
- Piloting
- Autonomous piloting
- Capacity
- Air cargo. 2 cubic meters (2 m3), (71 ft.3) cargo hold. The aircraft can hold two standard 80 cm X 120 cm X 14.4 cm (2 ft, 7.5 in X 3 ft, 11.2 in X 5.75 in) pallets or two transport containers. The cargo is loaded at the front of the aircraft.
- Cruise speed
- 180 km/h (112 mph)
- Range
- 1,000 km (621 m)
- Cruise altitude
- 4,000 m (13,123 ft)
- Empty weight
- 1,200 kg (2,646 lb)
- Maximum payload weight
- 300 kg (661 lb)
- Maximum takeoff weight
- 1,500 kg (3,307 lb)
- Propellers
- 9 propellers (8 VTOL propellers, 1 pusher propeller)
- Electric motors
- 9 electric motors
- Power source
- Internal combustion engine and battery packs
- Fuselage
- Carbon fiber composite
- Aircraft dimensions
- 11 m width X 7.2 m length X 2.0 m height (36 ft, 1 in width X 23 ft, 7-1/2 in length X 6 ft, 6-3/4 in)
- Wing
- 1 high wing (11 m, 36 ft, 1 inch)
- Tail
- 1 inverted V tail
- Landing gear
- Fixed skid landing gear
- Area needed to land
- 17 X 17 m (55 ft, 9.25 in X 55 ft, 9. 25 in)
- 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 passengers or cargo. 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 no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.