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Two satellites A and B move round the ea...

Two satellites A and B move round the earth in the same orbit. The mass of B is twice the mass of A.

A

Speeds of A and B are equal

B

The potential energy of earth +A is same is that of earth +B

C

The kinetic energy of A and B are equal

D

The total energy of earth +A is same as that of earth +B

Text Solution

AI Generated Solution

The correct Answer is:
To solve the problem, we need to analyze the motion of the two satellites A and B around the Earth. Let's break down the solution step by step: ### Step 1: Understand the problem We have two satellites, A and B, that are orbiting the Earth in the same orbit. The mass of satellite B is twice that of satellite A. We need to analyze their speeds, potential energy, kinetic energy, and total energy. ### Step 2: Determine the speed of the satellites The speed \( v \) of a satellite in orbit is given by the formula: \[ v = \sqrt{\frac{GM}{r}} \] where: - \( G \) is the gravitational constant, - \( M \) is the mass of the Earth, - \( r \) is the radius of the orbit (distance from the center of the Earth to the satellite). Since both satellites A and B are in the same orbit, they have the same radius \( r \). Therefore, their speeds will be: \[ v_A = \sqrt{\frac{GM}{r}} \quad \text{and} \quad v_B = \sqrt{\frac{GM}{r}} \] This shows that the speeds of satellites A and B are equal: \[ v_A = v_B \] ### Step 3: Analyze the potential energy The gravitational potential energy \( U \) of a satellite in orbit is given by: \[ U = -\frac{GMm}{r} \] For satellite A, the potential energy \( U_A \) is: \[ U_A = -\frac{G M m_A}{r} \] For satellite B, the potential energy \( U_B \) is: \[ U_B = -\frac{G M m_B}{r} = -\frac{G M (2m_A)}{r} = -\frac{2G M m_A}{r} \] Thus, the potential energy of satellite B is not equal to that of satellite A. ### Step 4: Analyze the kinetic energy The kinetic energy \( KE \) of a satellite is given by: \[ KE = \frac{1}{2} mv^2 \] For satellite A, the kinetic energy \( KE_A \) is: \[ KE_A = \frac{1}{2} m_A v_A^2 \] For satellite B, the kinetic energy \( KE_B \) is: \[ KE_B = \frac{1}{2} m_B v_B^2 = \frac{1}{2} (2m_A) v_B^2 = m_A v_B^2 \] Since \( v_A = v_B \), we have: \[ KE_B = m_A v_A^2 \] This shows that the kinetic energies of A and B are not equal. ### Step 5: Analyze the total energy The total energy \( E \) of a satellite in orbit is given by: \[ E = KE + U \] For satellite A: \[ E_A = KE_A + U_A = \frac{1}{2} m_A v_A^2 - \frac{G M m_A}{r} \] For satellite B: \[ E_B = KE_B + U_B = m_A v_B^2 - \frac{2G M m_A}{r} \] Since both kinetic and potential energies depend on the mass, the total energies will also differ. ### Conclusion From the analysis: - The speeds of satellites A and B are equal. - The potential energies of A and B are not equal. - The kinetic energies of A and B are not equal. - The total energies of A and B are not equal. Thus, the correct answer is that the speeds of A and B are equal.
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