东四平台卫星热试验中的关键技术

Key technologies of thermal test for DFH-4 platform satellite

东四平台系列卫星对真空热试验期间的星上转发器在轨工作状态模拟、星表高/低热流模拟、星体吊装与水平支撑和污染控制等提出了较高要求。文章对微波负载能量耗散试验技术、红外灯阵设计、液氮冷板设计、卫星吊装与支撑技术、污染控制及星内真空度监测技术等在该系列卫星热试验中的成功应用与完善进行了分析、总结。

In the thermal test for the DFH-4 platform satellite, high technical requirements have to be met for the on-orbit operating state simulation of the transponder, the high or low heat flux simulation for satellite’s surfaces, the satellite lifting and horizontal bracing, and the pollution control. This paper analyses the technologies for the energy dissipation of the microwave load, the design of the infrared lamp array, the design of the cold plate with liquid nitrogen, the satellite lifting and horizontal bracing, the vacuum degree monitoring inside the satellite and the contamination control, as well as the applications of above-mentioned technologies in test.