首页 | 本学科首页   官方微博 | 高级检索  
     

碳/氰酸酯复合材料原子氧效应试验研究
引用本文:翟睿琼, 田东波, 姜海富, 等. 碳/氰酸酯复合材料原子氧环境效应研究[J]. 航天器环境工程, 2018, 35(6): 1-1doi:10.12126/see.2018.06.010
作者姓名:翟睿琼  田东波  姜海富  武博涵  高鸿  李宇
作者单位:1.北京卫星环境工程研究所;2.中国航天宇航元器件工程中心:北京 100094
摘    要:
选取具有良好应用前景的M40/DFA-1、M40/DFA-N3(添加TiO2纳米颗粒)碳纤维增强氰酸酯基复合材料为研究对象,开展航天器在轨原子氧环境地面模拟试验,通过表面/断口形貌观察、质量损失测试、层间剪切强度测试以及表面成分分析等方式,分析探讨了上述2种碳/氰酸酯基复合材料的原子氧损伤效应。结果表明,在原子氧的作用下,2种材料表面树脂均受到了一定程度的剥蚀,添加纳米颗粒的M40/DFA-N3质损率及原子氧剥蚀率相对更高,但层间剪切强度下降幅度相对较小,这可能是由于其氧化反应更加剧烈,生成的碳氧双键比例更高的结果。

关 键 词:碳纤维   氰酸酯   复合材料   原子氧   剥蚀   地面试验研究
收稿时间:2018-07-30
修稿时间:2018-11-26

The effects of atomic oxygen interaction with carbon/cyanate composites
ZHAI R Q, TIAN D B, JIANG H F, et al. Study on effects of atomic oxygen interaction with carbon/cyanate composites[J]. Spacecraft Environment Engineering, 2018, 35(6): 1-1doi:10.12126/see.2018.06.010
Authors:ZHAI Ruiqiong  TIAN Dongbo  JIANG Haifu  WU Bohan  GAO Hong  LI Yu
Affiliation:1. Beijing Institute of Spacecraft Environment Engineering;2. China Aerospace Components Engineering Center: Beijing 100094, China
Abstract:
Two kinds of unidirectional laminates made of carbon/cyanate composite named M40/DFA-1 & M40/DFA-N3(nano TiO 2 contained) are selected for studying the effects of atomic oxygen interactions. Based on the ground simulation of atomic oxygen environment, several tests are conducted, such as the surface/fracture morphology observation, the mass loss test, the inter-laminar shear strength test, and the X-ray photoelectron analysis of surface components. After the exposure of 1.5×1020 cm-2 atomic oxygen, the surface detachment is observed on both types of materials. In addition, the mass loss as well as the erosion rate are calculated. It is shown that the M40/DFA-N3 sample exhibits relatively higher mass loss and erosion rate while with a smaller decrease of the inter-laminar shear strength compared with the specimens made of M40/DFA-1. It can be partly attributed to the drastic oxidation reaction within the nano TiO2 granules, which leads to a higher proportion of C=O bonds generated.
Keywords:carbon fiber  cyanate  composite materials  atomic oxygen  erosion  ground test study
本文献已被 CNKI 等数据库收录!
点击此处可从《航天器环境工程》浏览原始摘要信息
点击此处可从《航天器环境工程》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号