Centripetal Acceleration of a satellite above a planet of the Earth's radius.

AI Thread Summary
The discussion focuses on calculating the speed and orbital period of a satellite orbiting a planet with the same radius and gravitational acceleration as Earth. The initial attempt at solving the problem incorrectly assumed a one-year orbital period, leading to an erroneous speed calculation. The correct approach involves using the centripetal acceleration formula, where the gravitational force equals the centripetal force acting on the satellite. The final calculations yield a speed of approximately 7.9 km/s and a time for one complete orbit based on this speed. The conversation emphasizes the importance of using the correct parameters and formulas for accurate results.
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Homework Statement


A satellite is in orbit just above the surface of a spherical planet which has the same radius as Earth and the same acceleration of free fall at it's surface. Calculate:
i) Speed
ii) Time for 1 complete orbit.

Radius of Earth = 6400km or 6400000m and accel. of free fall = 9.81ms-2

Homework Equations


Speed (v) = (2pi)r/T

Cent. Accel. (a) = v2/r

Cent. Force. F = mv2/r = mw2r

The Attempt at a Solution



First time on here so finding it difficult to locate symbols so sorry for loss in translation.

My attempt of a solution is: v = (2xpi)x 6400000/3.1e7 (no of s in 1 year (365.25days))

v = 1.29ms-1
then plugged this into v2/r but this is heading down a blind alley.
Please Help.
 
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If you can't use LaTeX, "^" is standard for powers. Or [ sup]2[/sup] (without the first space).

Why would you believe "v = (2xpi)x 6400000/3.1e7" Are you assuming the satellite takes one year to orbit the planet?

The simplest thing to do is to calculate the centripetal force on the satellite- that is just the force holding in orbit which is just the gravitational force on the satellite:
F= -\frac{GmM}{r^2}
"G" and "M" are those values for the Earth and m is the mass of the satellite, r is 6400 km.

And then, of course, F= ma so
a= -\frac{GM}{r^2}

Now, on the surface of the earth, the acceleration due to gravity is -9.81 and the radius is, to two significant figures, 6400 km! Adding another 6400 for the altitude of the satellite, we have r= 2(6400) so r^2= 4(6400)^2.
 
hi mogsplanet! welcome to pf! :smile:

(try using the X2 icon just above the Reply box :wink:)
mogsplanet said:
My attempt of a solution is: v = (2xpi)x 6400000/3.1e7 (no of s in 1 year (365.25days))

v = 1.29ms-1
then plugged this into v2/r …

what does the year have to do with it? :confused:

as usual, use good ol' https://www.physicsforums.com/library.php?do=view_item&itemid=26" F = ma …

what is the acceleration? what is the force? :wink:
 
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The question has no mention of mass so this should not be used. All the information I have is in the original question. It is A satellite in low orbit around a planet with same radius as the Earth.
 
Thanks for help. It has come to me now.

9.81 = v^2/6400000

So v = 7.9e3 ms-1

and so time for 1 orbit is (2pi)r/v
 
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