Efficiency of Hysteresis Rods in Small Spacecraft Attitude Stabilization

Table 4

Properties of magnetic materials used in studied satellites.

Material	𝜇𝑖(Tm/A)	𝜈(T(m/A)^2)
AEM-4750	8.5×10^−3	3.95×10^−4
Mo-Permalloy	2.5×10^−2	1.1×10^−2
Permenorm	(3.8,12.6)×10^−3	(4.1×10^−4,1.55)