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The force of gravity on any object due to the earth is given by the equation F =(GmM/r^2), where (blah, blah, blah) and r is the distance of between the center of the mass of the earth and the center of the mass of the object. If a rocket weighs 3.6x 10^6 N at the surface of the earth, what is the force on the rocket due to the gravity when the rocket has reached an altitude of 1.2x 10^4km? (radius of earth= 6370 km)
A. 1.2x10^5N
B.4.3x10^5N
C. 4.8x10^6N
D.9.6x10^6N
EK's explanation: "If you are good with scientific notation, it is easy to see that r is tripled. r is the distance from the center of the Earth to the earth's surface. The Satellite is 2 Earth radii from the surface of the Earth so it is three earth radii from the center of the earth. Since the square of r is inversely proportional to F, F must be divided by 9."
Can somebody help me see HOW r is being tripled? I'm having a brain fart or something...
A. 1.2x10^5N
B.4.3x10^5N
C. 4.8x10^6N
D.9.6x10^6N
EK's explanation: "If you are good with scientific notation, it is easy to see that r is tripled. r is the distance from the center of the Earth to the earth's surface. The Satellite is 2 Earth radii from the surface of the Earth so it is three earth radii from the center of the earth. Since the square of r is inversely proportional to F, F must be divided by 9."
Can somebody help me see HOW r is being tripled? I'm having a brain fart or something...