Electrical Architecture of the Recovery System of a High Powered Rocket with Payload

In this study, a recovery system design is presented for a high-powered rocket, which can carry and place a payload that performs scientific value experiments up to any altitude, as well as recovering flight data, and providing safe recovery of both the rocket and the payload. Rescue systems were designed, individually tested and integrated as a dual deployment with the drogue parachute opening at the apogee and the main parachute opening at lower altitude. However, the presented system is a reusable recovery mechanism that reduces consumed materials and speeds up the preparation process. This design engineering builds an infrastructure to improve the system by making a positive contribution to future studies and eliminating the shortcomings of past studies with an overview of the advantages and disadvantages of various systems.