Title :
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
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;
Conference_Titel :
Circuits and Systems (MWSCAS), 2011 IEEE 54th International Midwest Symposium on
Conference_Location :
Seoul
Print_ISBN :
978-1-61284-856-3
Electronic_ISBN :
1548-3746
DOI :
10.1109/MWSCAS.2011.6026542
