Launch Velocity for Satellite from Mt. Everest to Orbit Earth

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To launch a satellite from the top of Mt. Everest into a circular orbit, it requires a specific horizontal velocity, which can be calculated using the formula for orbital velocity. The gravitational acceleration at the summit is 9.77 m/s², and the altitude is 8,850 meters, which affects the orbital dynamics. The satellite remains in orbit due to the balance between gravitational force and centripetal force. Understanding these forces and their calculations is crucial for determining the necessary launch velocity. The discussion emphasizes the need for clarity on the orbital velocity equation and the forces involved in maintaining orbit.
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At what horizontal velocity would a satellite have to be launched from the top of Mt. Everest to be placed in a circular orbit around the earth?

The book earlier in the chapter provides two things relating to Mt. Everest:
1. g at the top of Mt. Everest is 9.77 m/s2
2. The top of Mt. Everest according to the book is 8850 m

Unfortunately, I honestly have no idea how to begin to do this problem, and all of my buddies in physics are as perplexed as I am.

Thank you to anyone who helps!
Anthony
 
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The circular orbital velocity of a satellite is?
If you know that, the answer is just of substitute and solve.
 
I don't understand what you mean... :/
 
just that, do you know the formula for orbital velocity of a satellite?
 
I don't, I don't believe our teacher ever went over anything like that and our book is super vague. What is the orbital velocity of a satellite equation?
 
Do you know why a satellite stays in orbit? It is in equilibrium between two forces. If you know what those two forces are then you need to know how to calculate their strength in order for them to be in equilibrium?
 
Well there's the force of gravity pulling inwards, but there's no such thingas centrifugation in terms of force so I have no idea
 
cubejunkies said:
I don't, I don't believe our teacher ever went over anything like that and our book is super vague. What is the orbital velocity of a satellite equation?

I won't tell you that, but you know that there's a centripetal force acting on the satellite caused by gravitation.
What is the magnitude of centripetal force in terms of m,v,r(r being Radius of earth+Height)? and magnitude of gravitational force according to Newton's law of gravitation?

Equate them ...
jumble with the equation until you get v that is the orbital velocity.
 
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