Prototype of CanSat with Auto-gyro Payload for Small Satellite Education

This paper is about structure and payload for CanSat. The structure on CanSat must fit on a space rocket and protect the payload from all disruption. The structure made from PLA+ carbon fiber that makes it light and strong. On the structure, there is a blade for descent control that makes CanSat down slowly. The payload on CanSat was chosen by a mission that CanSat brings a sensor accurately. Mission on this CanSat is descent control with science payload. The payload that fit with structure and can operate well. The main contribution of this paper is a proposed structure and payload that can be a reference for other CanSat. Our results on this research are structure and payload can operate the mission with small damage on structure.