A 400kg satellite is in a circular orbit of radius 2R about the earth.Calculate the energy needed to transfer it to a circular orbit of radius 4R.Find the changes in it's kinetic energy and it's potential energy (Given R=6400km radius of earth g=10m/s sq.)
Answers
Explanation:
Given A 400 kg satellite is in a circular orbit of radius 2R about the earth. Calculate the energy needed to transfer it to a circular orbit of radius 4R. Find the changes in it's kinetic energy and it's potential energy (Given R=6400 km radius of earth g=10m/s sq.)
- Given m = 400 kg, R = 6.4 x 10^6 m
- Initial total energy = Potential energy + kinetic energy
- = - Gmm /r + 1/2 mVo^2
- = - Gmm / r + 1/2 m((√Gm / r)^2
- = - Gmm/2r
- = - Gmm / 2(2R)
- = - Gmm / 4R
- So final total energy = - Gmm / 2r
- = - Gmm / 2(4R)
- = - Gmm / 8R
- So change in total energy will be
- ΔE = Ef – Ei
- = – Gmm / 8R - (- Gmm / 4R)
- = Gmm / 8R
- Solving further we get
- Gm / (R)^2 x m R / 8
- = gm R / 8
- We know acceleration due to gravity will be g is 10 m / s
- = 10 x 400 x 6.4 x 10^6 / 8
- = 3.20 x 10^9 J is the required energy.
- So now decrease in kinetic energy
- K.E = Ki – Kf
- = 1/2 (Gm / 2R) – 1/2 m(Gm/4R)
- Δ K.E = GmR / 8 = 3.20 x 10^9 J
- Gain in potential energy is Uf – Uc
- = - Gmm / 4R – (- Gmm / 2R)
- = - Gmm / 4R
- Now solving gmR / 4
- = 10 x 400 x 6.4 x 10 ^6 / 4
- = 6.40 x 10^9 J
So gain in P.E is twice as loss in K.E
So P.E = - 2K.E
Reference link will be
https://brainly.in/question/4288837
The changes in it's kinetic energy and it's potential energy is
Given:
Mass = m = 400 kg
Radius = R = 6400 km
Acceleration due to gravity = g = 9.8 m/s²
To find:
Kinetic energy and potential energy = ?
Solution:
Initial energy is given by the formula:
Final energy is given by the formula:
Change in kinetic energy and potential energy:
On substituting the known values, we get,
The Kinetic Energy will become half.
The Potential Energy will become twice.