宇航材料工艺2011，Vol.41Issue(5)：66-68,73,4.
490N远地点发动机抗氧化涂层厚度对性能的影响
Effect of Thickness on Oxidation Resistance of Coatings on 490 N Apogee Engine
周红玲 1徐方涛 2张绪虎 3贾中华3
作者信息
- 1. 国防科技大学航天与材料工程学院,长沙410073
- 2. 上海空间推进研究所,上海200233
- 3. 航天材料及工艺研究所,北京100076
- 折叠
摘要
Abstract
Modified silicide was used as high temperature oxidation resistant coatings on 2nd 490 N apogee engine thruster chamber, and its thickness affected the performance of coatings obviously. The life experiment of samples with different thickness was taken at 1 700℃ , and it was found that the best range of thickness was 140 to 160 μm. Available of lower thickness of SiO2 or to much of the amount of micro cracks and holes would shorten the lifetime.关键词
远地点发动机/高温抗氧化/涂层/硅化物Key words
Apogee engine/ High temperature oxidation resistance/ Coatings/ Silicide引用本文复制引用
周红玲,徐方涛,张绪虎,贾中华..490N远地点发动机抗氧化涂层厚度对性能的影响[J].宇航材料工艺,2011,41(5):66-68,73,4.
