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超高燃速推进剂的限燃包覆层 被引量:1

Inhibition of Very High Burning Rate Propellant
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摘要 研究了超高燃速推进剂的侧面限燃包覆。通过包覆层厚度、中止燃烧、间接证明实验,证实了采用硬质PVC黏合剂为内层,添加石棉粉的醋酸纤维素为外层的包覆层,可以使超高燃速推进剂侧面不发生窜火,达到稳定对流燃烧,燃速可达1000mm/s以上。 A novel propellant, which was of porous structure and had very high burning rate (above 1 000 mm/s), was prepared. Its inhibitor is very important in studying the application of very high burning-rate propellant. The propellant grains with size Φ 25×25 mm were inhibited using polyvinyl chloride (PVC) as inner layer and cellulose acetate added flake asbestos as outer layer. The experiment of determining the thickness of coating layer, termination burning and indirect proof were studied. Results show that the convection burning of VHBR propellant is stable, no flame-leak. Its burning rate is above 1 000 mm/s by using this way.
出处 《火炸药学报》 EI CAS CSCD 2004年第4期63-65,共3页 Chinese Journal of Explosives & Propellants
关键词 推进剂 超高燃速 限燃 包覆层 对流燃烧 propellant very high burning rate (VHBR) restricted combustion inhibitor convection burning
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  • 1[1]Fifer R A.Combustion of very high burning rate propellants[R].AD-A 121 668,1982.
  • 2[2]Kooker D E,Anderson R D.The two-phase flow burning mechanisms of very high burning rate propellants[R].AD-A 111 248,1981.
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  • 4李晓东,杨荣杰,李建民,何吉字.超高燃速推进剂燃速压力敏感性理论探讨[J].火炸药学报,2003,26(3):24-26. 被引量:2

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