A satellite of mass orbits a spherical planet of radius with surface gravitational acceleration . The satellite is transferred from an initial circular orbit of radius to a higher circular orbit of radius . What is the minimum energy required, in megajoules (), to perform this transfer?
Answer: 2500 MJ
Answer
The minimum energy required to perform the orbital transfer is .
The minimum energy needed to move a satellite between circular orbits is equal to the change in its total mechanical energy (). Expressing as , the energy difference between radii and simplifies to , which evaluates to .
Step-by-Step Solution
Key Concept
Total Mechanical Energy of a Satellite in Circular Orbit and Orbital Transfer Energy
Estimated Time:3m 0s