DocumentCode :
113857
Title :
Electromagnetic compatibility of MARS Orbiter Mission spacecraft
Author :
Raghavaiah, Vaddi ; Sowjanya, P. ; Mini, R.L. ; Murthy, P.V.N. ; Muniraja, S.M. ; Renuka, R. ; Murali, G. K. Rama ; Binu, D. ; Sankaranarayanan, Santhi ; Kumar, V. Senthil ; Srinivas, B.S. ; Hariharan, V.K. ; Srinivasan, V.V.
Author_Institution :
ISRO Satellite Centre, Bangalore, India
fYear :
2014
fDate :
15-17 Dec. 2014
Firstpage :
209
Lastpage :
212
Abstract :
The MARS Orbiter Mission (MOM) spacecraft carries on-board sensitive receiver and high gain antenna system to cater to the requirement of inter-planetary and deep space communication. This paper describes, among others, the stringent EMC requirements for MOM spacecraft, summary of EMC analysis carried out, modification on subsystem level EMI/EMC test limit and EMI/ESD mitigation techniques followed to achieve EMC compliance of MOM Spacecraft.
Keywords :
artificial satellites; electromagnetic compatibility; interference suppression; radio receivers; satellite antennas; space communication links; EMC analysis; EMC requirements; EMC test limit; EMI mitigation technique; ESD mitigation technique; MARS Orbiter Mission spacecraft; MOM spacecraft; deep space communication; electromagnetic compatibility; high gain antenna system; interplanetary communication; on-board sensitive receiver; Antenna measurements; Electromagnetic compatibility; Electromagnetic interference; Electrostatic discharges; Mars; Method of moments; Space vehicles; EMI/EMC/ESD; Mars Orbiter Mission Spacecraft;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Microwave and RF Conference (IMaRC), 2014 IEEE International
Conference_Location :
Bangalore
Type :
conf
DOI :
10.1109/IMaRC.2014.7039009
Filename :
7039009
Link To Document :
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