Respuesta :
Answer:
(A) The distance of the center of Planet X is [tex]6.18 \times 10^{7}[/tex] m
(B) The speed of the satellite is [tex]898.38 \frac{m}{s}[/tex]
Explanation:
Given:
Mass of the planet [tex]m = 7.5 \times 10^{23}[/tex] kg
Time period [tex]T = 5[/tex] days [tex]= 432000[/tex] sec
(A)
From kepler's third law
[tex]T^{2} = \frac{4\pi ^{2}r^{3} }{Gm}[/tex]
Where [tex]G = 6.67 \times 10^{-11}[/tex]
Now for finding the distance of planet X,
[tex]r^{3} = \frac{Gm T^{2} }{4\pi ^{2} }[/tex]
[tex]r^{3} = \frac{6.67 \times 10^{-11} \times 7.5 \times 10^{23 } \times (432000) ^{2} }{4 (3.14)^{2} }[/tex]
[tex]r^{3} = 236 \times 10 ^{21}[/tex]
[tex]r = (236 \times 10^{21} )^{\frac{1}{3} }[/tex]
[tex]r = 6.18 \times 10^{7}[/tex] m
(B)
Speed of the satellite is given by,
[tex]v = \frac{2\pi r}{T}[/tex]
[tex]v = \frac{6.28 \times 6.18 \times 10^{7} }{432000}[/tex]
[tex]v = 898.38[/tex] [tex]\frac{m}{s}[/tex]
Therefore, the speed of planet is [tex]898.38 \frac{m}{s}[/tex]
The motion of the satellite around the hypothetical Planet X is described
by Kepler's laws of planetary motion.
(a) The distance from the center of the center of Planet X at which the
satellite would remain in one spot is approximately 61852641 meters.
(b) The speed of the satellite is approximately 899.6 m/s
Reasons:
The given parameters are;
Mass of Planet X, M = 7.5 × 10²³ kg.
Number of times the plane rotates every 5 days = Once
(a) The period of the satellite around a planet is given by the formula;
According to Kepler's third law of planetary motion, we have;
[tex]T^2 \propto r^3[/tex]
[tex]T^2 = \left(\dfrac{4 \cdot \pi ^2}{G \cdot M} \right) r^3[/tex]
Therefore;
[tex]r = \sqrt[3]{\dfrac{T^2 \cdot G \cdot M}{4 \cdot \pi^2} }[/tex]
Where;
T = 5 days = 432,000 seconds
G = The universal gravitational constant = 6.67430 × 10⁻¹¹ N·m²/kg²
Which gives;
[tex]r = \sqrt[3]{\dfrac{432000^2 \times 6.67430 \times 10^{-11} \times 7.5 \times 10^{23}}{4 \cdot \pi^2} } \approx 61852641[/tex]
The distance from the center of the center of Planet X at which the satellite
would remain in one spot, r ≈ 61852641 meters
(b) The angular speed of the satellite, ω, is given as follows;
[tex]\omega = \dfrac{2 \cdot \pi}{432000} \ rad/s[/tex]
The linear speed, v = ω × r
Therefore;
[tex]v = \omega = \dfrac{2 \cdot \pi}{432000} \times 61852641 \approx 286.35 \cdot \pi \approx 899.6[/tex]
The speed of the satellite, v ≈ 899.6 m/s
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