Home
Class 12
PHYSICS
Assume that Earth is in circular orbit a...

Assume that Earth is in circular orbit around the Sun with kinetic energy K and potential energy U, taken to be zero for infinite separation. Then, the relationship between K and U:

A

is K=U

B

is K = −U

C

is K = U/2

D

is K = −U/2

Text Solution

AI Generated Solution

The correct Answer is:
To find the relationship between the kinetic energy (K) and potential energy (U) of the Earth in a circular orbit around the Sun, we can follow these steps: ### Step 1: Understand the Forces Acting on Earth The Earth is in a circular orbit around the Sun, which means that the gravitational force between the Earth and the Sun provides the necessary centripetal force for the Earth's circular motion. ### Step 2: Write the Expression for Centripetal Force The required centripetal force (F_c) for an object moving in a circular path is given by: \[ F_c = \frac{mv^2}{r} \] where: - \( m \) is the mass of the Earth, - \( v \) is the orbital velocity of the Earth, - \( r \) is the radius of the orbit (distance from the Earth to the Sun). ### Step 3: Write the Expression for Gravitational Force The gravitational force (F_g) between the Earth and the Sun is given by Newton's law of gravitation: \[ F_g = \frac{GMm}{r^2} \] where: - \( G \) is the gravitational constant, - \( M \) is the mass of the Sun, - \( m \) is the mass of the Earth, - \( r \) is the distance between the centers of the Earth and the Sun. ### Step 4: Set the Centripetal Force Equal to the Gravitational Force For the Earth to remain in a stable circular orbit, the centripetal force must equal the gravitational force: \[ \frac{mv^2}{r} = \frac{GMm}{r^2} \] ### Step 5: Cancel Out Mass and Rearrange We can cancel \( m \) from both sides (assuming \( m \neq 0 \)): \[ \frac{v^2}{r} = \frac{GM}{r^2} \] Rearranging gives: \[ v^2 = \frac{GM}{r} \] ### Step 6: Calculate Kinetic Energy (K) The kinetic energy (K) of the Earth in its orbit is given by: \[ K = \frac{1}{2} mv^2 \] Substituting \( v^2 \) from the previous step: \[ K = \frac{1}{2} m \left(\frac{GM}{r}\right) = \frac{GMm}{2r} \] ### Step 7: Calculate Potential Energy (U) The gravitational potential energy (U) of the Earth-Sun system is given by: \[ U = -\frac{GMm}{r} \] ### Step 8: Relate Kinetic Energy to Potential Energy From the expressions derived: - Kinetic Energy: \( K = \frac{GMm}{2r} \) - Potential Energy: \( U = -\frac{GMm}{r} \) Now, we can express the kinetic energy in terms of potential energy: \[ K = -\frac{1}{2} U \] ### Conclusion Thus, the relationship between the kinetic energy (K) and potential energy (U) of the Earth in a circular orbit around the Sun is: \[ K = -\frac{1}{2} U \]

To find the relationship between the kinetic energy (K) and potential energy (U) of the Earth in a circular orbit around the Sun, we can follow these steps: ### Step 1: Understand the Forces Acting on Earth The Earth is in a circular orbit around the Sun, which means that the gravitational force between the Earth and the Sun provides the necessary centripetal force for the Earth's circular motion. ### Step 2: Write the Expression for Centripetal Force The required centripetal force (F_c) for an object moving in a circular path is given by: \[ F_c = \frac{mv^2}{r} \] ...
Promotional Banner

Similar Questions

Explore conceptually related problems

For a satellite moving in an orbit around the earth, ratio of kinetic energy to potential energy is

For a satellite moving in a circular orbit around the earth, the ratio of its potential energy to kinetic energy is

The relationship between kinetic energy (K) and potential energy (U) of electron moving in a orbit arund the nucleus is

An artificial satellite moving in a circular orbit around the earth has a total energy E_(0) . Its potential energy is

For a satellite moving in a circular orbit around the earth, the ratio of its total mechanical energy to kinetic energy

An artificial moving in a circular orbit around the earth has total mechanical energy E_(0) . Its kinetic energy is

A satellite is moving with constant speed V in a circular orbit around earth. The kinetic energy of the satellite is

An artificial satellite moving in circular orbit around the earth has total (kinetic + potential) energy E_(0) . Its potential energy and kinetic energy respectively are :