摘要
准确计算局部—线性—顺序分流器的发热功耗是确定该分流器温控措施及计算其温度范围的前提。本文就该分流器发热功耗的组成进行分析,并给出发热功率与卫星负载功率关系的表达式;然后,对一个典型的分流器的发热功耗进行计算。
Accurate calcutation of heat produced by the partial-linear-sequential shunt is the basis of its thermal control design.In present paper the components of heat produced by the current shunt have been analysed and an expression on the relation between heat produced and load power in satellite has been given, finally, heat produced by a typical partiallinear-sequential shunt has been calculated a relation curve between heat produced and load po wer in satellite has been show.
出处
《中国空间科学技术》
EI
CSCD
北大核心
1990年第2期64-70,共7页
Chinese Space Science and Technology
关键词
通信卫星
航天电源
热负荷
功率损耗
Communication satellite, Space power system, Thermal load, Power loss, Calculation.