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  • 标题:Influence of Bicurative on Processibility of Composite Propellant
  • 本地全文:下载
  • 作者:S.N. Jawalkar ; Dr. Mehilal ; R. Kurva
  • 期刊名称:Defence Science Journal
  • 印刷版ISSN:0976-464X
  • 出版年度:2007
  • 卷号:57
  • 期号:5
  • 页码:669-675
  • DOI:10.14429/dsj.57.1800
  • 语种:English
  • 出版社:Defence Scientific Information & Documentation Centre
  • 摘要:A new series of composite propellant compositions, based on ammonium perchlorate,hydroxy-terminated polybutadiene and having metallic fuel as aluminium powder, have beendeveloped. Pressure cast-cum-cured compositions have also been developed with toluenediisocyanate (TDI), isophorone diisocyanate (IPDI), and a mixture of both curatives, i.e., TDIand IPDI, respectively, to study their effect on processibility, mechanical and ballistic propertiesof the compositions. The data indicate that the compositions based on bicurative have a potlife of 7 - 8 h, viscosity build up is from 13280 poise to 14080 poise after 4 h, and the smoothprocessibility of the slurry is enhanced. Further, the mechanical properties are in the range12.2 kg/cm2, 40.2 kg/cm2, and 40.2 per cent for tensile strength, E-modulus and elongation,respectively, and burn rate is almost the same, i.e., 16 ±0.5 mm/s.
  • 关键词:Composite propellants, ammonium perchlorate, bicurative, hydroxy-terminatedpolybutadiene, toluene diisocyanate
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