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Introduction Mars Orbiter Mission (MOM) is the maiden interplanetary mission of ISRO. The mission was conceived to be a technology demonstrator and includes five payloads which are designed for the observation of the physical features of Mars and its outer atmosphere. The MOM scientific payloads are supported by mainframe systems like power, thermal, communication system, control, digital, and propulsion systems. The electrical power system of MOM comprises of a single power bus tied to adoi:10.1051/e3sconf/20171604001 fatcat:6hoomrczfrezjbpyxc4sumhcke