A Method for Express Analysis of Mechanical, Erosion, and Contaminating Impact of Plasma Jet of Electric Propulsion Thruster onto the Large Object of Space Debris

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详细

A method for express analysis of mechanical, erosion and contaminating impact of plasma jet of an electric propulsion thruster onto the large object of space debris during its de-orbiting from a protected orbit to the disposal one is presented. The results of analytical and numerical calculations agree that verifies the method validity.

作者简介

S. Blyakharskii

Moscow Aviation Institute

Email: nadiradze@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

Ya. Blyakharskii

Moscow Aviation Institute

Email: nadiradze@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

A. Nadiradze

Moscow Aviation Institute

编辑信件的主要联系方式.
Email: nadiradze@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

R. Rakhmatullin

Moscow Aviation Institute

Email: nadiradze@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993


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