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同步定点轨道双自旋稳定卫星(以下简称同步自旋卫星)目前广泛应用于通信卫星和气象卫星。卫星总体结构方案设计牵涉面、综合性强,它不仅涉及卫星的总体方案和各分系统的方案及要求,而且涉及卫星所遇到的各种环境、地面试验以及与运载火箭的联接和分离等问题。该项设计技术也比较复杂,要把这项工作做好,必须进行广泛的调研、全面的分析和大量的计算,有时还需做必要的试验工作。除此之外,这项设计还包含大量的协调工作,其中包括缩比模型和1:1的模型工作。本文拟对同步自旋卫星总体结构方案设计进行综合概述。
Synchronous fixed-orbit dual-spin stable satellite (hereinafter referred to as synchronous spin satellite) is currently widely used in communications satellites and meteorological satellites. Satellites overall structure of the program design involves many comprehensive and strong, it not only involves the overall program of the satellite and subsystems programs and requirements, but also involves the satellite encountered a variety of environments, ground tests and with the launch vehicle connection and separation problem. This design technique is also quite complicated. To do a good job of this work, extensive research, comprehensive analysis and a large amount of calculation are necessary. In some cases, the necessary experimental work needs to be done. In addition, this design also includes a large number of coordination work, including the scale model and 1: 1 model work. This article intends to synchrotron satellite structure of the overall program design overview.