(Solved): Consider a spin-stabilized satellite in pure spin about its third axis with an angular momentum, \( ...

Consider a spin-stabilized satellite in pure spin about its third axis with an angular momentum, \( \mathrm{H}_{0} \), of 6000 N.m.s. We wish to reorient the satellite spin-axis by an angle of 60 degrees. What would be the total angular momentum change needed for the maneuver? Pick the appropriate equation for your calculation from the following: \[ \begin{array}{l} \Delta \vec{H}=\vec{M} \cdot \Delta \mathrm{t} \\ \vec{H}_{1}=\vec{H}_{o}+\Delta \vec{H} \\ \Delta H_{\text {Total }}=2|\Delta \vec{H}|=2\left|\vec{H}_{o}\right| \tan \theta \\ 12000 \text { N.m.s } \\ \quad 6928 \text { N.m.s } \\ 9458 \text { N.m.s } \\ 20785 \text { N.m.s } \end{array} \]