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有机硅基耐烧蚀材料的研究
引用本文:邹德荣. 有机硅基耐烧蚀材料的研究[J]. 有机硅材料, 2001, 15(5): 12-14
作者姓名:邹德荣
作者单位:中国航天科技集团上海航天技术研究院第806所,
摘    要:以室温硫化硅橡胶为基材,采用联二脲、芳纶纤维作为配合剂制成了固体火箭发动机用耐烧蚀材料,讨论了联二脲和芳纶对材料烧蚀率和机械性能的影响。结果表明,联二脲、芳纶纤维单独和混合使用都能够降低烧蚀材料的烧蚀率。当以7.5/0.5的比例混合使用时,能够获得最低的烧蚀率(线烧蚀率和质量烧蚀率分别为0.146mm/s和0.153g/s)。由于联二脲、芳纶纤维与室温硫化硅橡胶的相容性较差,材料的机械性能有所下降。

关 键 词:固体火箭发动机 耐烧蚀材料 有机硅基 联二脲 芳纶 室温硫化硅橡胶
修稿时间:2001-07-02

Study on Property of Silicone- based Ablation Resistant Material
Zou Derong. Study on Property of Silicone- based Ablation Resistant Material[J]. Silicone Material, 2001, 15(5): 12-14
Authors:Zou Derong
Abstract:s:RTV rubber was used as basic material in the preparation of ablation material for solid rocket motor. LDA/ Kevlar were added to the ablation material. The ablation rate and mechanical property of the material were tested. The results showed that LDA/ Kevlar could decrease the ablation rate of the ablative material. The lowest ablation rate was made when bakelite/ asbestine were added together in a certain proportion. The mechanical properties decreased because of the bad compatibility between RTV rubber and filler.
Keywords:solid rocket motor  ablation material  silicone  LDA   Kevlar
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