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中燃速HTPB推进剂燃速公差控制
引用本文:唐承志,丁汝昆.中燃速HTPB推进剂燃速公差控制[J].固体火箭技术,1995,18(2):35-38.
作者姓名:唐承志  丁汝昆
作者单位:湖北襄樊四院四十二所
摘    要:研究了复合推进剂燃速公差控制的原理和方法,评估了固体组分粒度偏差和组分称量偏差地中燃速丁羟推进剂燃速公差的影响,结果表明,粒度偏差是导致燃速波动的主要原因,称量偏差的影响可忽略不计。

关 键 词:端羟基聚丁二烯  推进剂  燃速  粒度分布

Allowances Control of the Burning Rate of Moderate Burning Rate HTPB Propellant
Tang Chenzhi, Ding Rukun, Hou Cailan.Allowances Control of the Burning Rate of Moderate Burning Rate HTPB Propellant[J].Journal of Solid Rocket Technology,1995,18(2):35-38.
Authors:Tang Chenzhi  Ding Rukun  Hou Cailan
Abstract:The principle and method of the allowances control of composite solid propellant burins rate are researched. The effects of solid particle she deviation and ingnedieut weighing deristion on the burning rate allowances of moderate buning rate HTPB propellant are evacuated. The results show that the variation of burning rate is mainly due to the particle size deviation, and the effect of welshing deviation can be neglected.
Keywords:Hydroxy terminated polybutadiene Propellont propellant burning rate Size ditribution
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