A 500 kg satellite remains at the same location relative to a location on a Planet Mars that rotates on its axis. The distance from the center of the Planet Mars to the satellite is r = 3.03 x 107 m. (M Mars = 6.42 x 1023 kg, G 6.67 x 1011 kg1 m³/s?) (a) What is the equation used to calculate the orbital period, T of the satellite? 472 %3D GMMars 472 T2 = GMMars 47 T = GM Satellite (b) Calculate the orbital period, T of the satellite (your answer must be in 2 decimal places) Your answer is x 105 s c) What is the equation used to calculate the speed of satellite?

A 500 kg satellite remains at the same location relative to a location on a Planet Mars that rotates on its axis. The distance from the center of the Planet Mars to the satellite is r = 3.03 x 107 m. (M Mars = 6.42 x 1023 kg, G 6.67 x 1011 kg1 m³/s?) (a) What is the equation used to calculate the orbital period, T of the satellite? 472 %3D GMMars 472 T2 = GMMars 47 T = GM Satellite (b) Calculate the orbital period, T of the satellite (your answer must be in 2 decimal places) Your answer is x 105 s c) What is the equation used to calculate the speed of satellite?

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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Concept explainers

Centripetal Force

A particle, body, object or certain mass while travelling in a rotational path or semicircular path, experiences an inertia force. If that inertia force pulls the towards the inward of the imaginary circle in the rotation, it is termed as centripetal force.

Question

A 500 kg satellite remains at the same location relative to a location on a Planet Mars that rotates on
its axis. The distance from the center of the Planet Mars to the satellite is r = 3.03 x 107 m.
(M Mars = 6.42 x 1023 kg, G = 6.67 x 1011 kg 1 m3/s2
%3D
(a)
What is the equation used to calculate the orbital period, T of the satellite?
472
T3 =
%3D
GMMars
472
T2 =
73
GM Mars
%3D
472
%3D
GM Satellite
(b) Calculate the orbital period, T of the satellite
(your answer must be in 2 decimal places)
Your answer is
x 105 s
(c) What is the equațion used to calculate the speed of satellite?
G MMars

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