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偶氮四唑胍对含催化剂的RDX-CMDB推进剂燃烧性能的影响研究

蔚红建 王琼 陈春林

固体火箭技术2012,Vol.35Issue(1):93-98,6.
固体火箭技术2012,Vol.35Issue(1):93-98,6.

偶氮四唑胍对含催化剂的RDX-CMDB推进剂燃烧性能的影响研究

Study on the influences of guanidinium azotetrazolate on combustion characteristics of RDX-CMDB propellants containing catalysts

蔚红建 1王琼 1陈春林2

作者信息

  • 1. 西安近代化学研究所,西安710065
  • 2. 泸州北方化学工业有限公司,泸州646605
  • 折叠

摘要

Abstract

Samples of RDX-CMDB propellents containing catalysts with RDX replaced by guanidinium azotetrazolate ( GZT) were prepared using slurry casting technique. The influences of GZT on combustion behaviors of RDX-CMDB propellants including burning rates, pressure exponents and flame structure were studied, and the reasons for the difference of combustion behaviors between propellants with catalysts and without catalysts were analyzed. The thermal behaviors of propellants were analyzed through the difference scanning calorimeter( DSC). Results indicate that GZT has great effects on flame temperature, width of dark zone, numbers of lighting point on the combustion surfaces and temperature gradient of combustion surface to condensed phase. The burning rates of propellants decrease with the increase in GZT content under pressure ranging from 1 Mpa to 10 Mpa,while pressure exponents increase. In the DSC curve of propellants containing GZT and catalysts, a new independent decomposition peak corresponding to decomposition of GZT appears, and the first decomposition peak temperature decreases with addition of GZT into propellant.

关键词

改性双基推进剂/偶氮四唑胍盐/燃烧性能/火焰结构/热行为

Key words

CMDB propellants/guanidinium azotetrazolate/combustion characteristics/flame structure/thermal behaviors

分类

航空航天

引用本文复制引用

蔚红建,王琼,陈春林..偶氮四唑胍对含催化剂的RDX-CMDB推进剂燃烧性能的影响研究[J].固体火箭技术,2012,35(1):93-98,6.

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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