Efficiency of Hysteresis Rods in Small Spacecraft Attitude Stabilization

Figure 9

Variation of the dissipated energy, 𝑊_ℎ, as a function of thickness, 𝑡, or diameter, 𝑑, of TFR and CCSRs for materials Fe₈₀B₁₀Si₁₀ and GO Fe-Si with length of 0.2 m, for different values of the peak applied field, 𝐻_𝑎. (a) CCSR, Fe₈₀B₁₀Si₁₀, (b) TFR, GO Fe-Si, (c) CCSR, GO Fe-Si, and (d) TFR, GO Fe-Si.

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(b)

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