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