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A89 Acylindrical rocketof diameter 2.0 mdevelops a spinaing motion in space of period 2.0s about the axis of the cylinder. To eliminate this spin two jet motors which are attached to the rocket at opposite ends of a diameter are fired until the spinning motion ceases. Each motor turns the rocket in the same direction and provides a constant thrust of 4.0 x 10'N in a direction tangential to the surface of the rocket and in a plane perpendicular to its axis. If the moment of inertis of the rocket about its . uylindeical axis is 60 x 10' kg m, caiculate the nunber of revolutions made by the rocket during the firing and the time for which the motors are fired.

A89 Acylindrical rocketof diameter 2.0 mdevelops a spinaing motion in space of period 2.0s about the axis of the cylinder. To eliminate this spin two jet motors which are attached to the rocket at opposite ends of a diameter are fired until the spinning motion ceases. Each motor turns the rocket in the same direction and provides a constant thrust of 4.0 x 10'N in a direction tangential to the surface of the rocket and in a plane perpendicular to its axis. If the moment of inertis of the rocket about its . uylindeical axis is 60 x 10' kg m, caiculate the nunber of revolutions made by the rocket during the firing and the time for which the motors are fired.

College Physics
College Physics
11th Edition
ISBN:9781305952300
Author:Raymond A. Serway, Chris Vuille
Publisher:Raymond A. Serway, Chris Vuille
Chapter1: Units, Trigonometry. And Vectors
Section: Chapter Questions
Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...
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A89 Acylindrical rocketof diameter 2.0mdevelops a spinaing metion in space of period 2.0s about the axis of the cylinder. To eliminate this spin two jet motors which are attached to the rocket at opposite ends of a diameter are fired until the spinning motion ceases. Each motor turns the rocket in the same direction and provides a constant thrust of 4.0 x 10'N in a direction tangertial te the surface of the rocket and in a plane perpendicular to its axis. If the moment of inertin of the rocket about its czlindeical axis is 6 0x 10° kg m, caiculate the nuniber of revolutions made by the rocket during the firing and the time for which the motors are fired.
Transcribed Image Text:A89 Acylindrical rocketof diameter 2.0mdevelops a spinaing metion in space of period 2.0s about the axis of the cylinder. To eliminate this spin two jet motors which are attached to the rocket at opposite ends of a diameter are fired until the spinning motion ceases. Each motor turns the rocket in the same direction and provides a constant thrust of 4.0 x 10'N in a direction tangertial te the surface of the rocket and in a plane perpendicular to its axis. If the moment of inertin of the rocket about its czlindeical axis is 6 0x 10° kg m, caiculate the nuniber of revolutions made by the rocket during the firing and the time for which the motors are fired.
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