Experimental substantiation of effectiveness of conception of artificial mini-magnetosphere as a means of spacecraft motion controlling in the Earth ionosphere

1Shuvalov, VA, 1Kuchugurnyi, Yu.P
1Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine, Dnipro, Ukraine
Space Sci.&Technol. 2018, 24 ;(2):43-46
https://doi.org/10.15407/knit2018.02.043
Section: Space and Atmospheric Physics
Publication Language: Russian
Abstract: 
We present briefly the project of space experiment “Spacecraft Mini-magnetosphere”.
       Concept of this experiment is proposed to substantiate the effectiveness of using an artificial mini-magnetosphere near the surface of a spacecraft as a means of controlling its motion in the Earth’s ionosphere due to the Lorentz force arising in the interaction in “spacecraft magnetic field - ionospheric plasma” system. A scheme with mini-magnetosphere can be used in space debris removal procedure by lowering orbits of debris parts causing them to get burnt in dense layers of the Earth's atmosphere.
Keywords: ionospheric plasma, Lorentz force, magnetic field, mini-magnetosphere, physical modeling, spacecraft movement control
References: 
1. Tokmak N. A., Kuchugurnyi Yu. P., Kochubei, G. S., Tsokur A. G. (2017). Mini-magnitosfera kak sredstvo upravleniya kosmicheskim apparatom v ionosphere Zemli [Mini-magnetosphere as a means of controlling a spacecraft motion in the Earth`s ionosphere]. Abstracts from 17 Ukrainska konferentsiya z kosmichnyh doslidzhen (21— 25 serpnya 2017 roku, Odesa) – 17 th Ukrainan conference on space research. (p. 223). Kiev: Akademperiodyka NAS Ukraine [In Russian].
2. Bombardelli C., Pelaez, J. (2011). Ion beam shepherd for contactless space debris removal. J. Guidance and Dynamics, 34 (3), 916—920.
https://doi.org/10.2514/1.51832
3. Kitamura S., Hayakawa Y., Kawamoto S. (2014). A reorbiter for large GEO debris objects using ion beam irradiation. Acta Astronautica, 94 (2), 725—735.
https://doi.org/10.1016/j.actaastro.2013.07.037
4. Nishida H., Funaki I. (2012). Analysis of thrust characteristics of a magnetic sail in magnetized solar wind. J. Propulsion and Power, 28 (3), 636—641.
https://doi.org/10.2514/1.B34260
5. Shuvalov V. A., Gorev N. B., Tokmak N. A., Kochubei, G. S. (2017). Physical simulation of the long-term dynamic action of a plasma beam on a space debris object. Acta Astronautica, 132, 97—102.
https://doi.org/10.1016/j.actaastro.2016.11.039
6. Shuvalov V. A., Priimak A. I., Bandel K. A., Kochubei G. S., Tokmak N. A. (2011). Heat exchange and deceleration of a magnetized body in a rarefied plasma flow. J. Applied Mechanics and Technical Physics, 52 (1), 1—8.
https://doi.org/10.1134/S0021894411010019
7. Shuvalov V. A., Tokmak N. A., Pismennyi N. I., Kochubei G. S. (2015). Control of the dynamic interaction of a “magnetized” sphere with a hypersonic flow of rarefied plasma. High Temperature, 53 (4), 463—469.
https://doi.org/10.1134/S0018151X15030177