雷达学报Issue(3)：301-306,6.DOI:10.3724/SP.J.1300.2013.13062
固态发射机热设计与飞行验证
Thermal Design and Flight Validation for Solid-state Transmitter
摘要
Abstract
Solid-state transmitter with large power and high heat flux is a key equipment of an HJ-1-C satellite;therefore, it has a great influence on satellite thermal design. Thermal design ensures that the solid-state transmitter works well within the allowable temperature limits of the equipment. The solid-state transmitter thermal design and solved key problems are provided in accordance with the HJ-1-C characteristics. Moreover, an analysis of satellites on orbit was performed. Based on the telemetry data, the thermal control design is shown to satisfy the temperature requirements of the solid-state transmitter.关键词
热设计/热试验/飞行验证/固态发射机Key words
Thermal design/Thermal test/Flight validation/Solid-state transmitter分类
信息技术与安全科学引用本文复制引用
王磊,耀普..固态发射机热设计与飞行验证[J].雷达学报,2014,(3):301-306,6.基金项目
国家重大科技专项工程资助课题 （）
