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基于硝化棉助燃的含能粘合剂爆热特征值测试研究

卢先明 段秉蕙 莫洪昌 徐明辉 刘宁

固体火箭技术2024,Vol.47Issue(3):364-369,6.
固体火箭技术2024,Vol.47Issue(3):364-369,6.DOI:10.7673/j.issn.1006-2793.2024.03.009

基于硝化棉助燃的含能粘合剂爆热特征值测试研究

Study on characteristic explosion heat of energetic binders by using nitrocotton(NC)as comburent

卢先明 1段秉蕙 1莫洪昌 1徐明辉 2刘宁2

作者信息

  • 1. 西安近代化学研究所,西安 710065
  • 2. 西安近代化学研究所,西安 710065||氟氮化工资源高效开发与利用国家重点实验室,西安 710065
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摘要

Abstract

Tests and studies were performed to characterize the energy properties of the target energetic binders,such as the combustion heat,enthalpies of formation and explosion heat characteristic values.The rationality of the energy properties as quanti-tative indexes for energy characterization of energetic binders were evaluated,and the method of using nitrocotton(NC)as combu-rent to test the explosion heat characteristic values of energetic binders was explored.The results show that when the mass ratio of energetic binder/NC reaches 1∶5,most energetic binders can be fully burned.The explosion heat characteristic value of energetic binder can be accurately measured by using nitrocellulose as the comburent.The explosion heat characteristic values of PGN and PVN measured by this method are 3164 kJ·kg-1 and 4713 kJ·kg-1,respectively,and the relative errors with the literature val-ues are less than 5%.The combustion heat can not accurately reflect the energy advantage of energetic binders.The energy charac-teristics of energetic binders can be well characterized by the explosion heat characteristic values,avoiding the self-contradictory of evaluation system caused by the difference between positive and negative enthalpy of formation.Under the condition of isolating oxy-gen,the energy contribution of energetic binders increase in the order of GETPE<FATPE<GAP<PBAMO<NC(12%)<PGN<PVN.

关键词

含能粘合剂/硝化棉/助燃法/爆热特征值/燃烧热/生成焓

Key words

energetic binders/nitrocotton/combustion-supporting method/characteristic explosion heat/heat of combustion/en-thalpies of formation

分类

航空航天

引用本文复制引用

卢先明,段秉蕙,莫洪昌,徐明辉,刘宁..基于硝化棉助燃的含能粘合剂爆热特征值测试研究[J].固体火箭技术,2024,47(3):364-369,6.

固体火箭技术

OA北大核心CSTPCD

1006-2793

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