The EMC analysis between COMS RE and the H II - a launcher RS

Author

Eui-Chan Kim ; Ja-Chun Koo ; Hak-Ju Lee

Author_Institution

Korea Aerosp. Res. Inst., Daejeon, South Korea

fYear

2011

fDate

7-10 Aug. 2011

Firstpage

1

Lastpage

3

Abstract

In this paper, the preliminary EMC analysis process between the Communication, Ocean and Meteorological Satellite (COMS) and Geostationary Earth Orbit (GEO) launch vehicles in the frequency range [1MHz-47GHz] is described. There are a lot of launchers for GEO in the world market. Those are ARIANE V, SEA LAUNCH, LAND LAUNCH, ATLAS III&V, DELTA IV, PROTON M/BREEZE M, SOTUZ, H II-A, ANGARA. In the paper the considered launch vehicle is PROTON, one of those launchers. The COMS satellite Radiated Emission (RE) specifications have been compared to H II-A launch vehicle Radiated Susceptibility (RS) limits. As a result, The radiated emission levels of COMS are not compliant with H II-A radiated susceptiblity limits.

Keywords

aircraft communication; electromagnetic compatibility; satellite communication; COMS RE; COMS satellite radiated emission specification; EMC analysis; GEO launch vehicle; H II - A launcher RS; PROTON; communication-ocean-and-meteorological satellite geostationary earth orbit; frequency 1 MHz to 47 GHz; radiated susceptibility limit; Earth; Electromagnetic compatibility; Electrostatic discharge; Satellites; Sensors;

fLanguage

English

Publisher

ieee

Conference_Titel

Circuits and Systems (MWSCAS), 2011 IEEE 54th International Midwest Symposium on

Conference_Location

Seoul

ISSN

1548-3746

Print_ISBN

978-1-61284-856-3

Electronic_ISBN

1548-3746

Type

conf

DOI

10.1109/MWSCAS.2011.6026542

Filename

6026542