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C/C喉衬材料烧蚀试验方法研究
引用本文:王书贤,陈林泉,刘勇琼.C/C喉衬材料烧蚀试验方法研究[J].固体火箭技术,2007,30(2):170-172.
作者姓名:王书贤  陈林泉  刘勇琼
作者单位:中国航天科技集团公司四院设计部,西安,710025
摘    要:C/C喉衬材料的烧蚀性能与原材料性能、工艺过程有很大关系,采用小型试验发动机可有效进行C/C喉衬材料烧蚀性能模拟试验。介绍了3种小型发动机喉衬烧蚀试验方法,并着重分析了一种方形喉衬的试验方法。试验结果表明,该方法适于各类喉衬材料的烧蚀性能对比,尤其适用于径棒法编织的C/C喉衬材料。

关 键 词:C/C喉衬材料  烧蚀试验方法  方形喉衬
文章编号:1006-2793(2007)02-0170-03
收稿时间:2005-11-01
修稿时间:2006-02-27

Investigation on ablative property test methods for C/C throat insert material
WANG Shu-xian,CHEN Lin-quan,LIU Yong-qiong.Investigation on ablative property test methods for C/C throat insert material[J].Journal of Solid Rocket Technology,2007,30(2):170-172.
Authors:WANG Shu-xian  CHEN Lin-quan  LIU Yong-qiong
Abstract:Ablative property of C/C throat insert has close relations with raw material property and processing.Ablative property simulation test of C/C throat insert can be effectively carried out by means of small-scale test motor.Three ablative test methods for small-scale motors were introduced,and a new test method for quadrate throat insert was emphatically analyzed.Test results show that this method is applicable for ablative properties comparison of various kinds of throat insert material,especially C/C throat insert weaved with radial carbon rod.
Keywords:C/C throat insert  ablative test method  quadrate throat insert
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