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Whenever two apollo astronauts were on the surface of the moon, a third astronaut orbited the moon. assume the orbit to be circular and 430 km above the surface of the moon, where the acceleration due to gravity is 1.08 m/s2. the radius of the moon is 1.70 â 106 m?

User Tim Kuehn
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Missing question:
"Determine (a) the astronaut’s orbital speed v and (b) the period of the orbit"

Solution

part a) The center of the orbit of the third astronaut is located at the center of the moon. This means that the radius of the orbit is the sum of the Moon's radius r0 and the altitude (
h=430 km=4.3 \cdot 10^5 m) of the orbit:

r= r_0 + h=1.7 \cdot 10^6 m + 4.3 \cdot 10^5 m=2.13 \cdot 10^6 m
This is a circular motion, where the centripetal acceleration is equal to the gravitational acceleration g at this altitude. The problem says that at this altitude,
g=1.08 m/s^2. So we can write

g=a_c= (v^2)/(r)
where
a_c is the centripetal acceleration and v is the speed of the astronaut. Re-arranging it we can find v:

v= √(g r)= √((1.08 m/s^2)(2.13 \cdot 10^6 m))=1517 m/s = 1.52 km/s

part b) The orbit has a circumference of
2 \pi r, and the astronaut is covering it at a speed equal to v. Therefore, the period of the orbit is

T= (2 \pi r)/(v) = (2\pi (2.13 \cdot 10^6 m))/(1517 m/s) =8818 s = 2.45 h
So, the period of the orbit is 2.45 hours.
User Fbiville
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