Given: A satellite is launched into a circular orbit of radius \( R \) around the Earth. A second satellite is launched into an orbit of radius \( 1.03R \). We are asked to find how much larger the time period of revolution of the second satellite is compared to the first one.
The time period \( T \) of a satellite in a circular orbit around a planet is given by Kepler's third law, which can be expressed as: \[ T = 2\pi \sqrt{\frac{R^3}{GM}}, \] where: - \( T \) is the time period of revolution, - \( R \) is the radius of the orbit, - \( G \) is the gravitational constant, and - \( M \) is the mass of the Earth. This formula shows that the time period is proportional to the \( 3/2 \) power of the orbit radius: \[ T \propto R^{3/2}. \]
Let \( T_1 \) be the time period of the first satellite with orbit radius \( R \), and \( T_2 \) be the time period of the second satellite with orbit radius \( 1.03R \). Using the proportionality, we can write: \[ \frac{T_2}{T_1} = \left(\frac{R_2}{R_1}\right)^{3/2} = \left(\frac{1.03R}{R}\right)^{3/2} = (1.03)^{3/2}. \]
Now, calculate \( (1.03)^{3/2} \): \[ (1.03)^{3/2} \approx 1.045. \] Therefore, the time period of the second satellite is approximately 1.045 times the time period of the first satellite, or about a 4.5% increase. \[ \text{Percentage increase} = 1.045 - 1 = 0.045 \times 100 = 4.5\%. \]
The time period of revolution of the second satellite is larger than the first one approximately by \( \boxed{4.5\%} \).
Match the LIST-I with LIST-II
LIST-I (Energy of a particle in a box of length L) | LIST-II (Degeneracy of the states) | ||
---|---|---|---|
A. | \( \frac{14h^2}{8mL^2} \) | I. | 1 |
B. | \( \frac{11h^2}{8mL^2} \) | II. | 3 |
C. | \( \frac{3h^2}{8mL^2} \) | III. | 6 |
Choose the correct answer from the options given below:
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