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bii17

  • 3 years ago

can someone help me in this question.. Find the velocity in m/s that a satellite must have to pursue a circular orbit at an altitude equal to earth radius.. TNX

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  1. A.Avinash_Goutham
    • 3 years ago
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    it''s a phy thing but i guess i l help u out initially potential + kinetic = kinetic + potential

  2. bii17
    • 3 years ago
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    yes it is a physics question.. but no one help me to answer that on that subject...

  3. bii17
    • 3 years ago
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    @A.Avinash_Goutham what happen nxt?

  4. A.Avinash_Goutham
    • 3 years ago
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    ok fine i gave u the wrong hint

  5. A.Avinash_Goutham
    • 3 years ago
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    centrifugal force is gravitational r8? so

  6. Algebraic!
    • 3 years ago
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    |dw:1348065386687:dw|

  7. bii17
    • 3 years ago
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    @Algebraic! what will happen nxt?

  8. Algebraic!
    • 3 years ago
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    Me = mass of earth r = radius of earth G = universal gravitational constant

  9. Algebraic!
    • 3 years ago
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    solve for V

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