Satellite moving in a stable circular orbit

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Homework Help Overview

The discussion revolves around a physics problem involving a satellite in a stable circular orbit around the Earth. The original poster attempts to calculate the satellite's speed, orbital period, and gravitational force at a specified height above the Earth's surface, using given constants and equations related to gravitational force and circular motion.

Discussion Character

  • Exploratory, Assumption checking, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss calculations related to gravitational force and centripetal acceleration, with the original poster expressing uncertainty about their results. Questions arise regarding the correctness of the study guide's answer and the importance of including units in calculations. Some participants suggest that errors may stem from unit conversions or mathematical operations.

Discussion Status

The discussion is ongoing, with participants providing feedback on the necessity of units in calculations. Some guidance has been offered regarding the importance of proper unit usage, but no consensus on the correct approach or solution has been reached yet.

Contextual Notes

There is a noted concern about the accuracy of the study guide's answer, and participants are exploring the implications of missing units in the original poster's calculations. The original poster is under time pressure due to an impending final exam.

ronartest
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Homework Statement


A 600kg satellite moving in a stable circular orbit about the Earth at a height of 4000km (G=6.67x10^-11 NM^2/kg^2, Re=6380km, Me=5.98x10^24kg).
Calculate the speed of the satellite at that height.
Calculate the orbital period (T), the time for one revolution
Calculate the gravity at height h=4000 km.


Homework Equations


Gravitational Force: F=Gm1m2/r^2
centripetal acceleration: a= v^2/r
Period (circular motion): T=2(pie)r/v


The Attempt at a Solution


calculated a gravitational force of 2221179013, plugged it into F=ma, which I came out as 2221179013=600a. Got an acceleration of 3701965.021=v^2/r, which came out to v2= 3701965.02*10380. After taking the square root of that, I finished with v=196026.52m/s, which is off from the correct answer which is 6198.9 m/s. Where did I go wrong, how can I take the right steps? Thanks so much.
 
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I've been working on this question for a couple hours now and I can't seem to get a different answer. Is it possible that the answer given in the study guide is incorrect?
 
I just need help for the velocity part. I have a final on this tomorrow, can someone please help me find the error in my calculation? Thanks.
 
Your calculation is pretty much meaningless to me because you don't have any units attached to your numbers. I can't tell what error you might have made unless you have the proper units on each value.

For what it's worth, I was easily able to confirm the answer in the study guide, about 6.2 km/s.
 
You nailed it diazona (well, almost. It would have helped if ronartest had shown some work.)

Units, ronartest! These quantities are not just numbers.
 
Yay! Finally someone who cares as much as I do about units ;-)
 
Haha, yeah I'm really sorry about that. To be honest, I'm not really sure of the units on anything except the initial numbers. That said for the gravitational force I multiplied NM^2/kg^2 by kg by kg divided by km, whatever that comes out to. I guess the acceleration would be m/s^2. Is it not possible to understand the steps I am taking? Would it be possible to explain the steps that you took to achieve your answer? Again, I'm sorry for not being more clear, and I greatly appreciate your interest.
 
Would you attempt to do this problem without knowing how to multiply? Because that's just what you did. You really can't expect to be able to solve physics problems without knowing how to do basic math, and that includes both numbers and units.

So what are the units on the gravitational force you calculated?
[tex]F = G\frac{m_1 m_2}{r^2}[/tex]
You're right that G has units of N m^2/kg^2 (it's lowercase m for meters, not capital M), and both m1 and m2 have units of kilograms, and that r has units of kilometers (but note that r is squared in the denominator). How would you figure out the result of multiplying (N m^2/kg^2) * kg * kg / km^2?
 

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