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Aerospace Times Feipeng Co., LTD. (Feipeng) · China

FP-981C Sagittarius

Aerospace Times Feipeng FP-981C Sagittarius

升力+巡航 · 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
Cargo only, has bomber bay cargo doors so it can drop off cargo autonomously without ground crew being present
乘客
未公开/未录入
驾驶方式
Autonomous (or remote)
航程(按来源口径)
100 km (62 m)
巡航速度
100-130 km/h (62-81 mph)
最大速度
未公开/未录入
最大起飞重量
460 kg (1,014 lb)
载荷
100 kg (220 lb)
空重
360 kg (794 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
Batteries
电机
9 electric motors
旋翼/螺旋桨
9 propellers (8 VTOL propellers, 1 pusher propeller)
续航时间
1 hour
飞行高度
4,000 m (13,123 ft)
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.

全部原始参数

Specifications:

Aircraft type
Long-range air cargo eVTOL production model drone
Piloting
Autonomous (or remote)
Capacity
Cargo only, has bomber bay cargo doors so it can drop off cargo autonomously without ground crew being present
Cruise speed
100-130 km/h (62-81 mph)
Range
100 km (62 m)
Flight time
1 hour
Cruise altitude
4,000 m (13,123 ft)
Maximum altitude
4,500 m (14,764 ft)
Empty weight
360 kg (794 lb)
Maximum payload
100 kg (220 lb)
Maximum takeoff weight
460 kg (1,014 lb)
Propellers
9 propellers (8 VTOL propellers, 1 pusher propeller)
Electric motors
9 electric motors
Power source
Batteries
Fuselage
Carbon fiber composite
Wings
1 main high wing
Tail
1 high boom mounted horizontal stabilizer
Landing gear
Fixed skid 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.