The document summarizes the design and implementation of a communication and control system for an EDF rocket that uses remote sensing with a multi-client ground station. The purpose is to design and implement a rocket that can be used for remote sensing and controlled manually or automatically to its destination while sending parameter information to the ground station via wireless communication. Key aspects discussed include the basic theory of rockets, electric ducted fans, remote sensing, microcontrollers, and ground stations. The design and implementation section outlines the rocket mission, preparation of materials, mechanical design, payload and ground station communication design, rocket propulsion design, testing models and endurance testing, payload assembly and testing, propulsion installation and thrust testing, remote sensing system development, integration