标准摘要
[中文适用范围]： 本文件建立了对应用于航天器表面的热控制材料（TCMs）进行基于地面环境试验的要求和指南。 本文件描述了以下环境条件下的测试方法：带电粒子辐射、太阳紫外线（UV）、原子氧（AO）和温度循环。 本文件不涵盖其他环境影响，例如氙离子发动机羽流的污染效应（所谓的外部效应）或中子的影响（详细信息见附录B）。 本文件适用于典型的TCMs，包括但不限于油漆、二氧化硅、膜、阳极氧化物和玻璃（光学太阳反射器，OSR）。 本文件可用于其他适用类似要求的材料。 本文件致力于材料估算或评估试验，并可根据具体应用进行定制。 [外文原描述]： This document establishes requirements and guidance for the ground-based environmental testing of thermal control materials (TCMs) applied on spacecraft surface. This document describes the test methods for the following environmental conditions: charged particle radiation(s), solar ultraviolet (UV) radiation, atomic oxygen (AO) and thermal cycling. This document does not cover other environmental effects such as contamination effect of the Xenon ion engines plume (so called artificial effect) or the effects of neutron (see detailed information in Annex B). This document is applicable to typical TCM(s), including but not limited to, paint, silicate, film, anodic oxide, and glass (optical solar reflector, OSR). This document can be referenced for other materials, to which similar requirements apply. This document is devoted to material estimation or evaluation tests and can be tailored according to specific applications.
英文名称Space systems — Environmental testing for spacecraft thermal control materials