Instead of use r as the unknown radius, use r - △r because the statement given says:
Due to air drag, the radius of a satellite’s circular orbit decreases from r to r - △r, where the positive quantity △r is much less than r.
But maybe I'm wrong and the only way to demonstrate that the...
Hello, I have this problem statement : "Due to air drag, the radius of a satellite’s circular orbit decreases from r to r - △r, where the positive quantity △r is much less than r. The mass of the satellite is m. Show that the increase in orbital speed is △v = +(△r/2)[(GM/r^3)^1/2]; that the...
Yes, I've made the derivative of v respect r, but what I get it's:
v'= - (1/2)•[(GM/sqrt(GM/r^3)]
I'm pretty sure I've done something wrong because that isn't the solution given in the problem statement
Homework Statement
If a satellite is in a sufficiently low orbit, it will encounter air drag from the Earth's atmosphere. Since air drag does negative work (the force of air drag is directed opposite the motion), the mechanical energy will decrease. If E decreases (becomes more negative), the...