Email this article 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
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Affiliations:
- Moscow Aviation Institute
- Issue: Vol 62, No 4 (2019)
- Pages: 661-668
- Section: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/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.
About the authors
S. S. Blyakharskii
Moscow Aviation Institute
Email: nadiradze@mai.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
Ya. S. Blyakharskii
Moscow Aviation Institute
Email: nadiradze@mai.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
A. B. Nadiradze
Moscow Aviation Institute
Author for correspondence.
Email: nadiradze@mai.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
R. R. Rakhmatullin
Moscow Aviation Institute
Email: nadiradze@mai.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
