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A Study on Plume Disturbance Calculation Method of GEO-KOMPSAT-2 Satellite
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 Title & Authors
A Study on Plume Disturbance Calculation Method of GEO-KOMPSAT-2 Satellite
Kang, Wooyong; Chae, Jongwon; Park, Youngwoong;
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 Abstract
The attitude control, station keeping and wheel off-loading at GEO-KOMPSAT-2 are realized by thrusters firings. Thrusters 1, 2 and 3 are mounted on the same axis as the solar array, which generates the plume disturbance largely. Therefore the effect of plume disturbance should be analyzed from satellite design phase. In this paper, we described the calculation method of plume disturbance and analyzed the plume disturbance of thruster 1,2 and 3 using GEO-KOMPSAT-2 initial configuration.
 Keywords
GEO-KOMPSAT2;Plume;Disturbance;Thruster;Station keeping;Attitude control;
 Language
Korean
 Cited by
 References
1.
Choi J.D, Park J.S, Chang S.S, Park, B.K, Kim J.A, Lee S.R, "GEO-KOMPSAT2 Satellite Development Status", Autumn Conference of the Korean Society for Aeronautical and Space sciences, 2012, PP.864-869.

2.
Park Y.W, "Thruster Configuration Optimization on COMS and Preliminary Performance Analysis ", Korea Aerospace Research Institude, 2006, PP.114-118.

3.
Kang W.Y, Chae J.W, Park Y.W, Choi H.T, " Analysis of GEO-KOMPSAT-2 Satellite Plume Disturbance", Autumn Conference of the Korean Society for Aeronautical and Space sciences, 2013, PP.1448-1451.

4.
Chae J.W, Han J.Y, Jun H.Y, " A Technology Development of Dynamic Effects Analysis on Solar Arrays Due to Attitude Control Thruster's Plume of Geostationary Satellite", Autumn Conference of the Korean Society for Aeronautical and Space sciences, 2013, PP.1392-1395.

5.
Chae J.W, Han J.Y, Jun H.Y, " Dynamic Effects Analysis on a Solar Array Due to Attitude Control Thruster Plume", J. of The Korean Society for Aeronautical and Space Sciences 43(9), 799-804(2015). crossref(new window)