The invention relates to the technical field of overall design of spacecrafts, and discloses a multifunctional modularized spacecraft torque output system which comprises torque output equipment, an integrated support, a cable fixing clip and a module reference mirror. The integrated support is of a tower-shaped structure and comprises a support bottom plate and support side plates, and at least three sets of support side plates are arranged on the support bottom plate and form a pyramid tower-shaped structure. The torque output devices and the cable fixing clamps are arranged on the portions, located on the outer sides of the pyramid structures, of the support side plates. A module reference mirror is further arranged on the support bottom plate, and the module reference mirror and the support side plates are located on the two opposite end faces of the support bottom plate. The overall structure is simple and reliable, modular design is achieved, high pointing precision can be achieved, the module is overall convenient to disassemble and assemble, final assembly testing is facilitated, the overall satellite modular development level is improved, and the spatial orientation is easy to achieve.
本发明涉及航天器总体设计技术领域,公开了一种多功能模块化的航天器力矩输出系统,该系统包括力矩输出设备、一体化支架、线缆固定卡子和模块基准镜;所述一体化支架为塔型结构,包括支架底板和支架侧板,至少三组所述支架侧板设置在所述支架底板上,并形成棱锥塔型结构;每组所述支架侧板上并位于所述棱锥结构的外侧分别设置有所述力矩输出设备和电缆固定夹子;所述支架底板上还设置有模块基准镜,所述模块基准镜与所述支架侧板位于所述支架底板相对的两端面。本发明的整体结构简单、可靠,模块化设计并能实现高指向精度,模块整体拆装便捷,方便总装测试,提高整星模块化研制水平,空间方位也易实现。
Multifunctional modularized spacecraft torque output system
一种多功能模块化的航天器力矩输出系统
2024-01-09
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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