The Moon has a mass of M = 7.3 · 1022 kg, a radius of R = 1.7 · 106 m and a rotation period of
T = 27.3 days. Scientists are planning to place a satellite around the Moon that always remains
above the same position (geostationary).
(a) Calculate the distance from the Moon’s surface to this satellite.
(b) Explain if such a Moon satellite is possible in reality.
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Hey Dear,
◆ Answer -
h = 2.98×10^8 m
◆ Explanation -
# Given -
M = 7.3×10^22 kg
R = 1.7×10^6 m
T = 27.3 days = 2.36×10^6 s
# Solution -
(a)
Time period of geostationary satellite is given by -
T^2 = (R+h)^3 / GM
(2.36×10^6)^2 = (R+h)^3 / (6.67×10^-11 × 7.3×10^22)
(R+h)^3 = 5.57×10^12 × 4.87×10^12
(R+h)^3 = 2.712×10^25
R+h = 3×10^8 m
Distance of satellite from surface -
h = 3×10^8 - 1.7×10^6
h = 2.98×10^8 m
Therefore, distance of satellite from moons surface is 2.98×10^8.
(b)
Till date, no such geosynchronous satellite revolves around moon in reality.
Hope this helps..
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