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Satellite in Orbit

  1. Sep 19, 2011 #1
    Scientists want to place a 2500 kg satellite in orbit around Mars. They plan to have the satellite orbit a distance equal to 1.8 times the radius of Mars above the surface of the planet. Here is some information that will help solve this problem:

    mmars = 6.4191 x 1023 kg
    rmars = 3.397 x 106 m
    G = 6.67428 x 10-11 N-m2/kg2

    1)What is the force of attraction between Mars and the satellite?
    I got 2864.722760095893N but the online HW program says I am wrong and that I need to add one more radius. This is the formula I used: (2500(6.674282(10^-11))(6.4191(10^23)))/(1.8(3.397(10^6)))^2

    2)What speed should the satellite have to be in a perfectly circular orbit?

    No idea where to start with this one. Should I start with a free body diagram. I think I would have the W vector pointing in towards the center of mars and I would have to make the movement along the vertical axis (y) 0 and the movement along the horizontal axis (x) constant. Correct?
     
  2. jcsd
  3. Sep 19, 2011 #2
    This isn't a HW problem. I am just studying. I have spent a fair amount of time on this and can't get it right.
     
  4. Sep 19, 2011 #3

    berkeman

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    Staff: Mentor

    Welcome to the PF.

    You are correct to post here in the HH forums -- all schoolwork-type problems should be posted here. And it is good that you are showing your work.

    The questions uses the words "above the surface of the planet", so that's why you need to add in one radius of the planet to get your attractive force calculation based on the distance between the centers of mass of the two objects.

    And for the orbital speed, are you familiar with the equation(s) for uniform circular motion due to an attractive force?
     
  5. Sep 19, 2011 #4
    Q1: I plugged in a 2 for another radius and got this: (2500(6.674282(10^-11))(6.4191(10^23)))/(1.8(2(3.397(10^6))))^2 = 716.1806900239733. The answer seems to be incorrect again. puzzled. I must be reading something wrong.

    Q2: Uniform circular motion- so use centripetal acceleration (a=(v^2)/Radius)?
     
  6. Sep 19, 2011 #5

    berkeman

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    Staff: Mentor

    Q1: The satellite will be 1.8 times the radius of Mars *above* Mars. So the total distance is not 2*1.8 rmars.... What is it?

    (And there is no reason to show more than 3-4 digits past the decimal point in your answers.)

    Q2: Correct! Keep on going!
     
  7. Sep 19, 2011 #6
    Q1: simple. Thanks.

    Q2: Wow physics just baffles me. It's like magic. Lately it is just clicking for me and it never has until today. Knock on wood-I know it gets harder but it is a start. Thanks for your time.
     
  8. Sep 19, 2011 #7

    berkeman

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    Staff: Mentor

    Glad that it's starting to click, and glad to help. :smile:
     
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