Efficiency of Hysteresis Rods in Small Spacecraft Attitude Stabilization

Table 2

Demagnetization factor, 𝑁_𝑑, for different rod cross section shapes. 𝑒 is the elongation, 𝑤 the width of TFR, 𝑡 the thickness, all expressed in (m).

Shape	𝑁𝑑	Reference
CCSR	4.02log^𝑒10−0.1852𝑒^2	[16]
TFR	(0.057𝑤×10^3+0.2)𝑡	[5]