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A 6500 kg satellite orbits a planet. If its distance to the center of the planet is 9e6 m and its speed is 6.7e3 m/s, what is the gravitational force between the satellite and the planet

User Prudan
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2 Answers

2 votes

Complete Question

The complete question is shown on the first uploaded image

Answer:

Option D is the Answer

Step-by-step explanation:

The formula for the velocity of the satellite is


v =\sqrt{(GM)/(R) }

R is the distance to the center o the planet =
9*10^6m

G is the gravitational constant which is equal to
= 6.67*10^(-11) (Nm^2)/(kg^2)

M is the mass of the planet

Making M the subject of the formula we have


M = ((v^2)(R))/(G)


M = ((6.7*10^3)^2(9*10^6))/(6.67*10^(-11)) = 60.57*10^(23)Kg

The formula for the gravitational force between two object


F = (GMm)/(R^2)

Where


= (6.67*10^(-11)(6.057*10^(24))(6500))/((9*10^6)^2)


F = 32,419.90 N


= 3.24*10^(4) N

A 6500 kg satellite orbits a planet. If its distance to the center of the planet is-example-1
User Pedro M Duarte
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4.5k points
2 votes

Answer:

the gravitational force between the satellite and the planet is 32.4 * 10³N

Step-by-step explanation:

It is given that,

Mass of the satellite, m = 6500 kg

Speed of the satellite, v = 6.7 × 10³ m/s

distance to the center of the planet = 9 × 10⁶m

Let F is the magnitude of the gravitational force exerted on the satellite by the planet. The centripetal force is equal to the gravitational force. It is equal to :


F = (mv^2)/(R)


F = (6500 * (6.7 * 10^3))/(9 * 10^6)

= 32.4 * 10³N

the gravitational force between the satellite and the planet is 32.4 * 10³N

User Juwens
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