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  • 标题:Thermal Behaviour of AP Based CMDB Propellants with Stabilizers
  • 本地全文:下载
  • 作者:S. N. Asthana ; C. N. Divekar ; R. R. Khare
  • 期刊名称:Defence Science Journal
  • 印刷版ISSN:0976-464X
  • 出版年度:2013
  • 卷号:42
  • 期号:3
  • 页码:201-204
  • DOI:10.14429/dsj.42.4382
  • 语种:English
  • 出版社:Defence Scientific Information & Documentation Centre
  • 摘要:Stability test results and DTA studies indicate the superiority of molecular sieve (MS) over zirconium silicate (ZrSiO/sub 4/) as the stabilizer for a composite modified double base (CMDB) system. Shelf life as computed from autoignition test results was 30 years for MS-based composition which is almost double the life of ZrSiO/sub 4/, but approximately half the life of resorcinol-based composition which was used as a reference. Higher stabilizing effect of MS as compared to ZrSiO/sub 4/ has been explained on the basis of the presence of channels and cavities in its structure, which makes it an effective adsorbent for decomposition catalysing species. Poor stabilization capability of m-dinitrobenzene as compared to resorcinol suggests the catalytic involvement of acidic decomposition products of nitrate esters in autodecomposition process of CMDB propellants.
  • 关键词:Molecular sieve;Resorcinol based composition
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