Design and Development of Multi-Stage CANSAT for Measuring Attitude and Atmospheric Parameters

CanSat is a small soda CAN-size satellite used as a prototype model for the real satellite. The objective of this paper is to design and develop different CANSAT models. It includes preliminary as well as engineering designs. The basic methodology is to integrate all the subsystems to perform primary and secondary missions. This developed prototype performs some basic tasks that a real satellite performs. The design and mass budget are per the basic requirements applied for CanSat competitions. The aim is to promote space technology awareness in the education sector.