The satellite has a mass of 220 kg and a radius ofgyration about z axis of k₂ = 0.1 m, excluding the twosolar panels A and B. Each solar panel has a mass of15 kg and can be approximated as a thin plate. Thesatellite is originally spinning about the z axis at a constantrate w = 0.5 rad/s when = 90°. (Figure 1)Figure0.3 m0-90°1.5 m0.2 m<B1 of 1Part ADetermine the rate of spin if both panels are raised and reach the upward position, 0 = 0°, at the same instant.Express your answer using three significant figures.W₂ =SubmitVE ΑΣΦ↓↑Request Answer< Return to AssignmentvecProvide FeedbackĆ?rad/s

In this problem first we calculate the moment of inertia at both conditions and then apply the…

The satellite has a mass of 220 kg and a radius of gyration about z axis of k, = 0.1 m, excluding the two solar panels A and B. Each solar panel has a mass of 15 kg and can be approximated as a thin plate. The satellite is originally spinning about the z axis at a constant rate w₂ = 0.5 rad/s when 0 = 90°. (Figure 1) Part A Determine the rate of spin if both panels are raised and reach the upward position, 0 = 0°, at the same instant. Express your answer using three significant figures. VE ΑΣΦ | 11 | vec ?

The satellite has a mass of 220 kg and a radius of gyration about z axis of k, = 0.1 m, excluding the two solar panels A and B. Each solar panel has a mass of 15 kg and can be approximated as a thin plate. The satellite is originally spinning about the z axis at a constant rate w₂ = 0.5 rad/s when 0 = 90°. (Figure 1) Part A Determine the rate of spin if both panels are raised and reach the upward position, 0 = 0°, at the same instant. Express your answer using three significant figures. VE ΑΣΦ | 11 | vec ?

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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