Dynamic interaction of a spacecraft with rarefied plasma in motion under a “magnetic sail”

1Shuvalov, VA, 1Tokmak, NA, 2Tsokur, AG, 3Kochubey, GS
1Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine, Dnipro, Ukraine
2Institute of Technical Mechanics of the NAS of Ukraine and SSA of Ukraine, Dnipropetrovsk, Ukraine
3Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2014, 20 ;(3):14-21
https://doi.org/10.15407/knit2014.03.014
Section: Spacecrafts and Payloads
Publication Language: Russian
Abstract: 

It is shown that the change in the relative orientation of the vectors of own magnetic field and plasma flow velocity is an effective means to control the dynamic interaction in the “spacecraft — plasma” system. It allows one to achieve the mode of interaction with non-zero aerodynamic quality and, as a result, regimes of deceleration and acceleration of “magnetized”body in the hypersonic flow of rarefied plasma.

Keywords: interaction in the spacecraft-plasma system
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