SIMULASI DAN ANALISIS UJI FUNGSIONAL HOMING METEO PAYLOAD ROKET KOMPETISI

Abstract

All of homing meteo payload has passed the functional test consisting of static and dynamic test, before the flight test. The static test consists of G-Shock, Vibration and G-force to know the telecommand function when the payload it shaken with spinned, and stamped the shock as big as 6-G wich is similar to the condition when the rocket take off from the launcher. During the test, the function of telecommand must be good and data can transmit from the payload to the ground segment. Self run test is to controll the payload as an efford to reach the target that is 30 degre from north clockwise less then 20 second and locked. Then the motor has to push the payload shown by deviation from center point. Based on the testing criteria, from the 38 competition rocket tested these rockets can transmit the data to the ground segment. Key words: : Payload, Telecommand, 6-G