“捕鲸叉”助推器排出物的热力学和热化学参数
林蓉薇
摘要(Abstract)：
<正> 一、引言采用分析技术预测“捕鲸叉”火箭发动机排出羽烟和周围大气之间的热力学和热化学相互作用,以确定由此产生的各种化学产物及其浓度,从而能估定对空气特性的局部影响。当固体推进剂导弹诸如“捕鲸叉”发射时,热排出物在导弹后面形成云状物。羽烟和周围大气以综合方式(此方式在某种程度上取决于导弹参数,诸如燃烧室压力、推进剂组分、弹道和周围大气条件)相互作用。如果没有分析预测,那么可假定推进剂组分元素和空气
关键词(KeyWords)：
基金项目(Foundation):
作者(Author): 林蓉薇
DOI: 10.16338/j.issn.1009-1319.1983.s9.002
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