DocumentCode
2656428
Title
The preliminary EMC analysis between GEO satellite and the delta 4 launch vehicle
Author
Kim, Eui Chan ; Ja Chun Koo ; Ra, Sung Woong
Author_Institution
Korea Aerosp. Res. Inst., Daejeon, South Korea
fYear
2009
fDate
18-22 Oct. 2009
Firstpage
1
Lastpage
2
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 [1 MHz-47 MHz] is described. The considered launch vehicle is delta IV. The COMS satellite Radiated Emission (RE) specifications have been compared to delta 4 launch vehicle Radiated Susceptibility (RS) limits. As a result, the radiated emission levels of COMS are compliant with delta 4 RS limits.
Keywords
satellite communication; space vehicles; GEO satellite; Geostationary Earth Orbit launch vehicles; delta 4 launch vehicle; preliminary EMC analysis; radiated emission level; radiated emission specification; radiated susceptibility limits; Aluminum; Artificial satellites; Attenuation; Electromagnetic compatibility; Marine vehicles; Meteorology; Oceans; Payloads; Radio frequency; Underwater communication;
fLanguage
English
Publisher
ieee
Conference_Titel
Telecommunications Energy Conference, 2009. INTELEC 2009. 31st International
Conference_Location
Incheon
Print_ISBN
978-1-4244-2490-0
Electronic_ISBN
978-1-4244-2491-7
Type
conf
DOI
10.1109/INTLEC.2009.5351757
Filename
5351757
Link To Document