Mathematical simulation of ozonosphere perturbations in spacecraft launches

被引:0
|
作者
Yatsenko, OV [1 ]
机构
[1] Don State Tech Univ, Rostov Na Donu, Russia
关键词
Mathematical Model; Ozone; Chemical Agent; Mathematical Simulation; Kinetic Characteristic;
D O I
10.1023/B:RJAC.0000018682.83052.3d
中图分类号
O69 [应用化学];
学科分类号
081704 ;
摘要
Factorial analysis of the results obtained in numerical simulation of ozone layer depletion by spacecraft was carried out. The mechanism, chemical agents, and kinetic characteristics responsible for the dynamics of ozone level in the perturbed region were studied. A mathematical model of the processes, intended for engineering-ecological estimates, was suggested.
引用
收藏
页码:1776 / 1783
页数:8
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