Prototype Design & Development of an Autonomous Water-Powered Rocket with CanSat

This paper details the design and implementation of a prototype Can Satellite, featuring three essential components: the main body, ground station, and parachute mechanism for the ejection. This satellite is equipped with an automatic injection system powered by a water-based engine, highlighting a novel approach to sustainable aerospace technology. The main body integrates advanced functionalities for payload delivery and data collection, while the ground station acts as the operational hub for monitoring and controlling satellite activities. The parachute mechanism ensures a safe descent, facilitating precise landings for payload retrieval. This prototype demonstrates the feasibility of water-powered systems in aerospace applications, promoting environmentally friendly practices and offering promising solutions for future satellite missions in environmental monitoring and disaster response.