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 I. INTRODUCTION Analytical techniques are used to predict the thermodynamic and thermo-chemical interactions between the “catch whale” rocket engine to expel the plumes and the surrounding atmosphere to determine the resulting chemical products and their concentrations, Local effects of characteristics. When a solid propellant missile, such as a “whaling fork,” is fired, the hot exhaust forms a cloud behind the missile. The plume interacts with the surrounding atmosphere in an integrated manner, which depends to some extent on missile parameters such as combustor pressure, propellant composition, trajectory and ambient atmospheric conditions. If no analysis is predicted, then the propellant component elements and air may be assumed