User:ECE3SATwiki

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http://ece3sat.wikia.com/wiki/ECE3SAT_Wiki

PRESENTATION:
Nowadays, the earh orbit is becoming more and more full of space debris, most of them are located in the low earth orbit and the situationis getting worse in 2209 if nothing can not be done now.

There is a need for deorbiting systems for cubeSats.Thus, the solution is to provide a deorbiting system using Earth magnetic field, which has to be cost-efficient, roorm-efficient, and light in order to be easily implemented on other CubeSats missions.

TABLE OF CONTENTS:

 * Organisation of the project
 * EPS module
 * ADCS module
 * OBC module
 * TCS module