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

S. S. Blyakharskii; Ya. S. Blyakharskii; A. B. Nadiradze; R. R. Rakhmatullin

doi:10.3103/S1068799819040172

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

Authors: Blyakharskii S.S.¹, Blyakharskii Y.S.¹, Nadiradze A.B.¹, Rakhmatullin R.R.¹
Affiliations:
1. Moscow Aviation Institute
Issue: Vol 62, No 4 (2019)
Pages: 661-668
Section: Aircraft and Rocket Engine Theory
URL: https://journal-vniispk.ru/1068-7998/article/view/231179
DOI: https://doi.org/10.3103/S1068799819040172
ID: 231179

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Abstract

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.

Keywords

space debris object, service spacecraft, de-orbiting, plasma jet, electric propulsion thruster, mechanical impact, erosion impact, contaminating impact, express analysis method