Abstract
Factorial analysis of the results obtained in numerical simulation of ozone layer depletion byspacecraft was carried out. The mechanism, chemical agents, kinetic characteristics responsible for thedynamics of ozone level in the perturbed region were studied. A mathematical model of the processes, intended for engineering-ecological estimates, was suggested.
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Yatsenko, O.V. Mathematical Simulation of Ozonosphere Perturbations in Spacecraft Launches. Russian Journal of Applied Chemistry 76, 1776–1783 (2003). https://doi.org/10.1023/B:RJAC.0000018682.83052.3d
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DOI: https://doi.org/10.1023/B:RJAC.0000018682.83052.3d