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Many people assume air resistance acting on a moving object will always make the object slow down. It can, however, actually be responsible for making the object speed up. Consider a 180-kg Earth satellite in a circular orbit at an altitude of 205 km. A small force of air resistance makes the satellite drop into a circular orbit with an altitude of 80 km. (Use the following values: G = 6.67 10-11 m3 kg−1 s−2, mass of the Earth 5.98 1024 kg, radius of the Earth 6.37 106 m.)

User JordanBean
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Many people assume air resistance acting on a moving object will always make the object slow down. It can, however, actually be responsible for making the object speed up. Consider a 180-kg Earth satellite in a circular orbit at an altitude of 205 km. A small force of air resistance makes the satellite drop into a circular orbit with an altitude of 80 km. (Use the following values: G = 6.67 10-11 m3 kg−1 s−2, mass of the Earth 5.98 1024 kg, radius of the Earth 6.37 106 m.)

(a) Calculate the satellite's initial speed. m/s

(b) Calculate its final speed in this process. m/s

Answer:

a)
7.730*10^3m/s

b)
7.80*10^3m/s

Step-by-step explanation:

Given that;

The Earth satellite = 180-kg

altitude (radius r ) = 205 km

After the satellite drop into a circular orbit; the final altitude (r) = 80 km

G =
6.67 *10^(-11)m^3kg^(-1)s^(-2)

mass of the earth =
5.98*10^(24)kg

radius of the earth =
6.37 *10^(6)m

The original speed for both circular orbit is given as:


v = \sqrt{(GM_E)/(r) }

(a) Calculate the satellite's initial speed m/s


v = \sqrt{(6.67*10^(-11)*5.89*10^(24))/(6.37*10^6+205*10^3) }

v = 7729.88

v =
7.730*10^3m/s

b) Calculate its final speed in this process m/s


v = \sqrt{(6.67*10^(-11)*5.89*10^(24))/(6.37*10^6+80*10^3) }

v =7804.42


v =7.80*10^3m/s

User Ernist Isabekov
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