Abstract:

The design characteristics of a Space Satellite for a typical Telecom mission have not changed much in the last 30 years, with components breakdown made up by honeycomb panels, onto which variegate S/S Equipment are mounted, assembled around a central core comprising of the Sat fuel tank for orbital circularization in final orbit, the combustion chamber and its nozzle, and on the lateral sides of the cuboid structure the antennas and solar panels hinged to the structure.