Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 360 km above the earth's surface, while that for satellite_B is at a height of 720 km. Find the orbital speed for each satellite. 360 x 10°m 720 x 10°m Known: - 360km = r6 =720kn TA =?? To= ? For urrulau s ĜhM GM = v² Unknown: Strategy: V= 2nえT But 4222 3
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 360 km above the earth's surface, while that for satellite_B is at a height of 720 km. Find the orbital speed for each satellite. 360 x 10°m 720 x 10°m Known: - 360km = r6 =720kn TA =?? To= ? For urrulau s ĜhM GM = v² Unknown: Strategy: V= 2nえT But 4222 3
Classical Dynamics of Particles and Systems
5th Edition
ISBN:9780534408961
Author:Stephen T. Thornton, Jerry B. Marion
Publisher:Stephen T. Thornton, Jerry B. Marion
Chapter8: Central-force Motion
Section: Chapter Questions
Problem 8.37P
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Modeled after the two satellites problem (slide 12 in Lecture13, Universal gravity), imagine now if the period of the satellite is exact 93.55 hours, the earth mass is 5.98 x 1024 kg, and the radius of the earth is 3958.8 miles, what is the distance of the satellite from the surface of the earth in MILES? Use G=6.67x 10 -11 Nm2/kg2. Your answer for this problem is some large number on the order of 105 to 106. Just put in the raw number as your answer. For example, 34567.11.
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