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

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.