The invention relates to the technical field of spacecrafts, in particular to an attitude and orbit control system and an aircraft. The system is applied to the aircraft, the wall of an aircraft body of the aircraft is formed by connecting a main body on the inner side and a skin on the outer side, a flow channel extending from the head of the aircraft body to the tail of the aircraft body is arranged between the main body and the skin, and the system comprises a gas storage bottle, an attitude controller and a track booster, the outlet end of the gas storage bottle is communicated with the flow channel at the head position of the machine body, and the gas storage bottle is used for providing heat-conducting gas into the flow channel; the posture controller is arranged at the position between the head and the tail of the machine body, the posture controller communicates with the flow channel, and the posture controller is used for discharging gas in the flow channel out of the machine body; the rail booster is arranged at the tail of the machine body, communicates with the flow channel and is used for discharging gas in the flow channel out of the machine body. According to the technical scheme, the maneuverability of the aircraft can be improved.
本申请涉及空间飞行器的技术领域,特别是涉及一种姿轨控制系统及飞行器。该系统应用于飞行器,飞行器的机体的机壁由内侧的主体和外侧的蒙皮连接构成,主体与蒙皮之间设有自机体的头部向尾部延伸的流道,系统包括贮气瓶、姿态控制器以及轨道助推器,其中:贮气瓶内存储有加压的导热气体,贮气瓶的出口端与机体的头部位置的流道连通,贮气瓶用于向流道内提供导热气体;姿态控制器设于机体的头部与尾部间的位置,姿态控制器连通于流道,姿态控制器用于将流道内的气体排出至机体外;轨道助推器设于机体的尾部,轨道助推器连通于流道,轨道助推器用于将流道内的气体排出至机体外。采用本申请的技术方案可以提高飞行器的机动性。
Attitude and orbit control system and aircraft
一种姿轨控制系统及飞行器
27.05.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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