Saeed. Kosari Zade - Space Research Laboratory of Aerospace Faculty - Aerospace Faculty - Khajeh Nasireddin Toosi University of Technology
Ebrahim. Shirzadi - Space Research Laboratory of Aerospace Faculty - Aerospace Faculty
Mehran. Mirshams - Space Research Laboratory of Aerospace Faculty - Aerospace Faculty
Navid. Heidari - Mechatronics research Lab of Mechanic

In this paper, we have explained an operational method, and test procedure, which can be used to recognize, and evaluate accuracy of the magnetic dipole, and the generated torque by magnetorquers. This process is based upon usage of the satellite orbital magnetic surroundingssimulator system (Kosar 100).As in this manner all the external factors affecting the test results are eliminated by the mentioned system thereforethe results achieved are more accurate and reliable. On the other hand, this testing method can be used to develop (edit) characteristics ofnewfound materials in magnetic space scope as magnetorquer cores

Magnetic dipole moment, Magnetic field simulator, Space system testing equipment, Magnetorquer