Gravitational Forces acting on a satellite

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Homework Help Overview

The discussion revolves around gravitational forces acting on a satellite in orbit around the Earth. The problem involves calculating the gravitational force between the Earth and a weather satellite, as well as determining the satellite's orbital period, circumference, and speed.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss the application of gravitational force equations and circular motion concepts. There are attempts to calculate gravitational force and orbital parameters, with some participants expressing uncertainty about converting units and applying formulas correctly.

Discussion Status

Some participants have provided guidance on using Newton's second law and centripetal acceleration to approach the problem. There is an acknowledgment of the need for clarification on how to apply learned concepts to specific parts of the problem, particularly regarding unit conversions and calculations.

Contextual Notes

Participants are working within the constraints of a homework assignment, which may limit the information they can use or the methods they can apply. There is a noted lack of consensus on the best approach to solve parts of the problem.

Lyphta
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[SOLVED] Gravitational Forces

Homework Statement


A 1000 kg weather satellite is orbiting the Earth at a constant speed. It is 500 km above the Earth's surface. The Earth has a mass of 5.976 x 10^24 kg and a radius of 6370 km. (a) How much gravitational force exists between the Earth and the satellite? (b) How long does it take the satellite to go around the Earth once? (c) How are is that (measured in meters)? (d) how fast is the satellite moving (in m/sec)?


Homework Equations


F=G(m1 m2)/r^2
C=2πr
v=rω

The Attempt at a Solution


(a) F=6.67 x 10^-11 N.m^2/kg^2)((1000kg)(5.976 x 10^24 kg)/6870000 m^2)
= 8445.5 N

(b) I have no idea how to do this one with the numbers that was given... the answer is 94.49 min...

(c) C=2(π)(6870000 m)
= 4.32 x 10^7m

(d) all I know is to do v=rω. But I don't know what to plug in... the answer is 7617.1 m/sec
 
Last edited:
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i know that stuff on the website. the only thing i don't understand is how to apply it to part b and d because I'm not sure of how to convert them into minutes. and without that, i can't figure out how to find the velocity...
 
I would do part d before doing part b, actually. Since you already know the force acting on the satellite, you can use Newton's second law F=ma. The acceleration a is centripetal acceleration, the expression for which is given on the site provided by Kurdt.

Do you see what I mean?
 
oh yeah i got it! thanks!
 

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