An internal mechanism is used to maintain a constant angular rate 2=0.032 rad/s about the z-axis the spacecraft as the telescopicbooms are extended at a constant rate. The length I is varied from essentially zero to 2.5 m. The maximum acceleration to which thesensitive experiment modules P may be subjected is 0.0047 m/s². Determine the maximum allowable boom extension rate i.1Answer: i1.8 m1.8 mimm/s

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An internal mechanism is used to maintain a constant angular rate 2 = 0.032 rad/s about the z-axis of the spacecraft as the telescopic booms are extended at a constant rate. The length / is varied from essentially zero to 2.5 m. The maximum acceleration to which the sensitive experiment modules P may be subjected is 0.0047 m/s². Determine the maximum allowable boom extension rate i. Answer: I = Q 1.8 m1.8 m i mm/s

An internal mechanism is used to maintain a constant angular rate 2 = 0.032 rad/s about the z-axis of the spacecraft as the telescopic booms are extended at a constant rate. The length / is varied from essentially zero to 2.5 m. The maximum acceleration to which the sensitive experiment modules P may be subjected is 0.0047 m/s². Determine the maximum allowable boom extension rate i. Answer: I = Q 1.8 m1.8 m i mm/s

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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Question

An internal mechanism is used to maintain a constant angular rate 2=0.032 rad/s about the z-axis the spacecraft as the telescopic
booms are extended at a constant rate. The length I is varied from essentially zero to 2.5 m. The maximum acceleration to which the
sensitive experiment modules P may be subjected is 0.0047 m/s². Determine the maximum allowable boom extension rate i.
1
Answer: i
1.8 m1.8 m
i
mm/s

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