摘要
航天器热平衡试验是航天器研制过程中的一项重要试验。随着航天技术的发展,以及设计验证方法的改进,对航天器热平衡试验提出了新的要求。在总结以往实践的基础上,结合航天器的热控设计,根据既能满足设计验证的要求、又可以简化研制流程的原则,提出了存在的问题和研究重点。
The thermal balance test is an important test in the process of spacecraft development, and it faces new requirements with the development of space technology and the improvement of the design validation method. In this paper, the problems are discussed based on the experience of previous thermal balance tests for satellites, and it is shown that one must adhere to the principle of thermal control design and design validation.
出处
《航天器环境工程》
2007年第2期63-68,61,共6页
Spacecraft Environment Engineering
关键词
热平衡试验
航天器
thermal balance test
spacecraft
