Status of EPS Battery configuration finalized Solar panel layout –finalized Solar panel Substrate is ready for bonding EM – fabricated and Completed the Testing EM – integrated with OBC and tested FM- Version 1 available for integration with S/C Advanced FM – Design completed, Fabrication in progress. Pending activities Advanced FM –card fabrication in progress EPS Readiness for S/C integration – OCT 2013

1.Solar panel layout and panel bus bar layout drawing for the fabrication (1:1 drawing). 2.Electrical wiring diagram of the solar panels 3.Anodisation of spacecraft structural elements 4.Bonding of solar cells on the spacecraft structural elements (Side and TOP panels), wiring and testing of panels - This will be done by Solar panel division of ISAC 5.Availability of storage box for the panels - Solar cells have to be protected from damage during mechanical integration of the spacecraft and during handling till launch. 6.Fabrication of battery clamp and base plate 7.Finalisation of SNAP switch configuration and routing. – The interface with launch vehicle and type and location of SNAP switch 8. Flight EPS PCB fabrication & checking bare PCB 9.Wiring of EPS PCB 10.EPS card testing. 11.Integration of EPS with S/c (Solar panels and Card) 12.Space level thermal design for the improved EPS configuration Pending Activities – EPS