Design and Development of a Functional CANSAT Model for Atmospheric Data Collection

This paper presents the design and development of a functional Can sized Satellite(CANSAT) prototype focused on acquiring atmospheric data while demonstrating the feasibility and effectiveness of miniaturized satellite systems. The prototype incorporates a telemetry system for data collection and transmission to a ground station, employing reliable wireless communication protocols for real-time monitoring. Controlled velocity descent is achieved through careful parachute dimensioning and the integration of servo-actuated PID(Proportional-Integral-derivative) controlled fins for precise orientation control. The successful implementation of this prototype serves as a proof-of-concept for future miniaturized satellite missions, showcasing its capabilities in telemetry, communication, and controlled descent.