satellite thermal vacuum test

A thermal couple analysis method and a thermal vacuum test method for CZ-2C/ SD during launching Iridium satellite are described in detail.

介绍了火箭发射卫星过程中星箭热耦合分析和热真空试验两种设计方法，具体介绍了综合应用计算和试验两种方法完成CZ-2C/SD火箭发射铱星任务的热环境和热控设计工作。

Anti-disturbance design of infrared heating cage in vacuum thermal test for satellite

卫星真空热试验用红外加热笼抗热干扰设计

Thermal vacuum test provides an important reference for the thermal design of satellite-borne microwave module and for the optimal design of aerospace products.

热真空试验为星载微波组件的工程设计和优化航天产品提供了一条重要参考依据。

The design method of the satellite vacuum thermal test database is discussed in this paper.

真空热试验数据库是卫星环境工程数据库的一个重要组成部分。

The vacuum thermal test of a small satellite

某航天小卫星的真空热试验