Refined estimates of the effect of jet discharges from launch vehicles on the kinetics of the stratospheric ozone

Refined estimates of the effect of jet discharges from launch vehicles on the kinetics of the... The kinetic model of perturbations of the stratospheric ozone by propulsive jet discharges of modern launch vehicles was modified, which made it possible to refine theoretical estimates of the accompanying physicochemical processes and to improve the reliability and consistence of the basic parameters. The natural and artificial mechanisms of turbulent dissipation of the rocket trace in the stratosphere and their dependence on the altitude were taken into account. The mass-energy and specific characteristics of the propulsive jet discharges of rockets were factorized. The agents, factors, and mechanisms determining the scale, level, and dynamics of the perturbation of stratospheric ozone in launches of liquid-propellant launch vehicles were revealed and a small-scale kinetic-diffusion model was suggested for engineering estimates. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Russian Journal of Applied Chemistry Springer Journals

Refined estimates of the effect of jet discharges from launch vehicles on the kinetics of the stratospheric ozone

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Publisher
Nauka/Interperiodica
Copyright
Copyright © 2006 by Pleiades Publishing, Inc.
Subject
Chemistry; Chemistry/Food Science, general; Industrial Chemistry/Chemical Engineering
ISSN
1070-4272
eISSN
1608-3296
D.O.I.
10.1134/S107042720609014X
Publisher site
See Article on Publisher Site

Abstract

The kinetic model of perturbations of the stratospheric ozone by propulsive jet discharges of modern launch vehicles was modified, which made it possible to refine theoretical estimates of the accompanying physicochemical processes and to improve the reliability and consistence of the basic parameters. The natural and artificial mechanisms of turbulent dissipation of the rocket trace in the stratosphere and their dependence on the altitude were taken into account. The mass-energy and specific characteristics of the propulsive jet discharges of rockets were factorized. The agents, factors, and mechanisms determining the scale, level, and dynamics of the perturbation of stratospheric ozone in launches of liquid-propellant launch vehicles were revealed and a small-scale kinetic-diffusion model was suggested for engineering estimates.

Journal

Russian Journal of Applied ChemistrySpringer Journals

Published: Oct 26, 2006

References

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