Rotary driving loading structure for laser chemical combined propeller

The invention relates to a rotary driving loading structure for a laser chemical combined propeller. The structure comprises a rotary disc, a rotary steering engine and at least two combustion rooms,wherein the rotary steering engine is connected to the rotary disc and is used for driving the rotary disc to rotate; the combustion rooms are hermetically and fixedly connected to the rotary disc, and the rotary disc rotates to drive the combustion rooms to rotate; each of the combustion rooms is provided with a solid propellant; and the combustion rooms are arranged in parallel, and the rotary steering engine is arranged parallel to the combustion rooms. The rotary driving loading structure for the laser chemical combined propeller provided by the invention is small in size and light in weight, and can meet the power demand on micro satellite orbit control. 本发明的用于激光化学联合推进器的旋转驱动装药结构包括转盘、旋转舵机和至少两台燃烧室；所述旋转舵机与所述转盘连接，所述旋转舵机用于驱动所述转盘转动；所述燃烧室与所述转盘密封固连，所述转盘的转动带动各燃烧室转动；各燃烧室装有固体推进剂；各台燃烧室相互平行布置，所述旋转舵机与所述燃烧室平行布置。本发明的用于激光化学联合