©2007, IIT Kanpur, All Rights Reserved
Power management system
with sufficient protection.
Surface-mounted solar
panels.
Rechargeable batteries.
Maintains the satellite withing
specified temperature limits.
Passive thermal control
system.
Separates the satellite from launch
vehicle interface between launch
vehicle and Jugnu.
Transmits beacon throughout the orbit.
Controls satellite and its payload.
Operates in full-duplex mode.
Tracks the satellite.
Payload and health-log data
acquisition.
Controls orientation of the satellite in
space.
Maintains stability and maneuvres for
imaging.
Sun tracking for maximum power.
Data handling.
Computation for other
subsystems.
System health log.
Payload operation.
Error handling and diagnosis.
Jugnu
IIT Kanpur Nanosatellite
