Change of Orbits A spacecraft in a circular orbit wishes to transfer to 6 another circular orbit of quarter the radius by means of a tangential thrust to move into an elliptical orbit and a second tangential thrust at the opposite end of the ellipse to move into the desired circular orbit. The orbits looks like below (the backwards case of the example we discussed in class). Find the thrust factors required and show that the speed in the final orbit is two times greater than the initial speed. P PP

University Physics Volume 1
18th Edition
ISBN:9781938168277
Author:William Moebs, Samuel J. Ling, Jeff Sanny
Publisher:William Moebs, Samuel J. Ling, Jeff Sanny
Chapter13: Gravitation
Section: Chapter Questions
Problem 9CQ: In the diagram below for a satellite in an elliptical orbit about a much larger mass, indicate where...
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Change of Orbits A spacecraft in a circular orbit wishes to transfer to
6
another circular orbit of quarter the radius by means of a tangential thrust to move into
an elliptical orbit and a second tangential thrust at the opposite end of the ellipse to
move into the desired circular orbit. The orbits looks like below (the backwards case of
the example we discussed in class). Find the thrust factors required and show that the
speed in the final orbit is two times greater than the initial speed.
P
PP
Transcribed Image Text:Change of Orbits A spacecraft in a circular orbit wishes to transfer to 6 another circular orbit of quarter the radius by means of a tangential thrust to move into an elliptical orbit and a second tangential thrust at the opposite end of the ellipse to move into the desired circular orbit. The orbits looks like below (the backwards case of the example we discussed in class). Find the thrust factors required and show that the speed in the final orbit is two times greater than the initial speed. P PP
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