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A satellite is projected horizontally (p...

A satellite is projected horizontally (parallel to the tangent on equator ) from a height of 150 km from the surface of earth , so that is moves in a circular orbit around earth. Then

A

initial velocity needed is `7.83 xx 10^3 m//s`

B

initial velocity needed is `11.745 xx 10^3 m//s`

C

time period of rotation of the satellite is around 1 hr 27 minutes

D

time period of rotation of the satellite is around 2 hr 10 minutes

Text Solution

AI Generated Solution

The correct Answer is:
To solve the problem step by step, we will calculate the initial velocity of the satellite and its time period of rotation. ### Step 1: Understand the Parameters - Height (h) of the satellite above the Earth's surface = 150 km = 150,000 m - Radius of the Earth (R) = 6400 km = 6,400,000 m - Mass of the Earth (M) = \(6 \times 10^{24}\) kg - Gravitational constant (G) = \(6.67 \times 10^{-11} \, \text{N m}^2/\text{kg}^2\) ### Step 2: Calculate the Distance from the Center of the Earth The total distance (R + h) from the center of the Earth to the satellite is: \[ R + h = 6,400,000 \, \text{m} + 150,000 \, \text{m} = 6,550,000 \, \text{m} \] ### Step 3: Use the Formula for Orbital Velocity The formula for the orbital velocity \(V_0\) of a satellite in a circular orbit is given by: \[ V_0 = \sqrt{\frac{GM}{R + h}} \] Substituting the known values: \[ V_0 = \sqrt{\frac{(6.67 \times 10^{-11}) \times (6 \times 10^{24})}{6,550,000}} \] ### Step 4: Calculate the Orbital Velocity Calculating the above expression: 1. Calculate \(GM\): \[ GM = 6.67 \times 10^{-11} \times 6 \times 10^{24} = 4.002 \times 10^{14} \, \text{m}^3/\text{s}^2 \] 2. Now substitute this into the velocity formula: \[ V_0 = \sqrt{\frac{4.002 \times 10^{14}}{6,550,000}} \approx \sqrt{6.11 \times 10^{7}} \approx 7.81 \times 10^{3} \, \text{m/s} \] ### Step 5: Calculate the Time Period of Rotation The time period \(T\) of the satellite can be calculated using the formula: \[ T = \frac{2\pi(R + h)}{V_0} \] Substituting the values: \[ T = \frac{2\pi \times 6,550,000}{7.81 \times 10^{3}} \] ### Step 6: Calculate the Time Period Calculating the above expression: 1. Calculate the circumference: \[ 2\pi \times 6,550,000 \approx 41,116,000 \, \text{m} \] 2. Now substitute this into the time period formula: \[ T \approx \frac{41,116,000}{7.81 \times 10^{3}} \approx 5,256 \, \text{s} \] ### Step 7: Convert Time Period to Minutes To convert seconds into minutes: \[ T \approx \frac{5256}{60} \approx 87.6 \, \text{minutes} \] This can be expressed as: \[ 1 \, \text{hour} + 27 \, \text{minutes} \] ### Final Answer - Initial velocity \(V_0 \approx 7.81 \times 10^{3} \, \text{m/s}\) - Time period \(T \approx 1 \, \text{hour} \, 27 \, \text{minutes}\)
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