Artificial mini-magnetosphere as a means of controlling spacecraft motion in the Earth ionosphere
Journal Title: Технічна механіка, Техническая механика, Technical Mechanics - Year 2018, Vol 2, Issue 2
Abstract
Based on the results of a series of experimental studies of the interaction of spacecraft models with a hypersonic rarefied plasma flow, this paper demonstrates the possibility of controlling spacecraft motion in the ionosphere with the use of a device of the “magnetic sail” type and proposes an idea of an experiment onboard a CubeSat microsatellite in a near-Earth orbit. If a spacecraft is equipped with a source of a strong magnetic field, then in a hypersonic rarefied plasma flow a nonuniform plasma structure called an artificial mini-magnetosphere, which is similar to a planetary magnetosphere, will form in the vicinity of the spacecraft. In this case, part of the plasma flow momentum will be transferred to the magnetic field source, thus resulting in additional forces acting on the spacecraft. This principle forms the basis for the “magnetic sail” – a jetless magnetohydrodynamic propul-sion unit that uses the kinetic energy of the solar wind. Experimental studies of the interaction of spacecraft mod-els with a plasma beam were conducted on a plasmaelectrodynamic setup. The drag and lift acting on the models were determined as a function of the flow parameters and the magnetic field. It was shown that an artificial mini-magnetosphere may be an effective means of controlling spacecraft motion in the Earth ionosphere. The experi-ment to be conducted in near-Earth space envisages equipping a microsatellite with permanent magnets encased in a controllable enclosure that shields the magnetic field and determining the satellite orbit variations after re-moving the shield as a function of the magnetic field parameters. The experiment might be a first verification of the concept of the “magnetic sail” as a spacecraft propulsion unit. Controlling the motion of a “magnetized” body by using the long-term interaction of the body’s magnetic field with the ionospheric plasma may be the key component of a radically new technology for space debris removal from the ionosphere.
Authors and Affiliations
Yu. Kuchugurnyi, S. Kulagin, A. Tsokur
Keywords
Related Articles
- EP ID EP462469
- DOI -
- Views 110
- Downloads 0
Classification of aerodynamic systems for low Earth orbit space hardware deorbiting
The aim of this paper is to develop a classifier of aerodynamic systems for low Earth orbit space hardware deorbiting. Aerodynamic deorbiting systems are classified. A coding scheme for systems of this type is proposed....
Features of algorithms for computing the flow in the passage of a counter-pressure air intake
Air intake shape designing is the key problem in the development of a ramjet. The aim of this paper is to formulate an algorithm for on-the-fly computing of supersonic flow stagnation in the passage of an air intake at...
Conditions of optimal trajectory of vehicle motion when locating sensors in zone of emergency
The paper deals with a mathematical statement and solution of the problem for searching a condition of an optimal trajectory of the vehicle when the wireless network sensors are located in the zone of emergency. The cond...
Experimental investigations in flows of gas and gas-dispersion media relative to problems of improved energy efficiency of pipeline systems
Problems for experimental measuring hydraulic parameters of pipelines with closely-spaced joint welds and those for pneumatic transport of bulk material at an elevated pressure of the carrying gas are examined. Benches f...
Analysis of technologies for spacecraft removal from low earth orbits using onboard-produced electromagnetic and magnetic fields
The aim of this paper is to analyze the effectiveness of propulsion devices with permanent magnets as an alternative space debris deorbit system for low earth orbits. The paper considers current problems in the developme...