A 400kg satellite is in a circular orbit of radius 2R(e) about the earth. How much energy is required to transfer it to a circular orbit of radius 4R(e) ? what are the changes in the kinetic and potential energies?
Answers
The kinetic energy is reduced and it mimics ∆E, namely,
The change in potential energy is twice the change in the total energy, namely
Answer:
The kinetic energy is reduced and it mimics ∆E, namely,
The kinetic energy is reduced and it mimics ∆E, namely,△K=K
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f −K
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f −K i
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f −K i
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f −K i =−3.13×10
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f −K i =−3.13×10 9
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f −K i =−3.13×10 9 J.
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f −K i =−3.13×10 9 J.
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f −K i =−3.13×10 9 J.
The kinetic energy is reduced and it mimics ∆E, namely,△K=K f −K i =−3.13×10 9 J. The change in potential energy is twice the change in the total energy, namely