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
- 作者: Blyakharskii S.1, Blyakharskii Y.1, Nadiradze A.1, Rakhmatullin R.1
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隶属关系:
- Moscow Aviation Institute
- 期: 卷 62, 编号 4 (2019)
- 页面: 661-668
- 栏目: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/231179
- DOI: https://doi.org/10.3103/S1068799819040172
- ID: 231179
如何引用文章
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