I have a couple more questions on this topic. I hope someone can help me. Thanks a lot!
1) A space shuttle ejects a 1.2x10^3 kg booster tank so that the tank is momentarily at rest, relative to Earth, at an altitude of 2.0x10^3 km. Neglect atmospheric effects. How much work is done on the booster tank by the force of gravity in returning it to Earth's surface?
[The first thing I can think of is W=Fd(cos theta), but here the force of gravity is not constant so I can't use this formula. How can I find the work done by gravity, then?]
2a) Calculate the escape speed from the surface of the Sun: mass = 1.99x10^30 kg, radius = 6.96x10^8 m.
2b) What speed would an object leaving Earth need to escape from our solar system?
[For 2a), I got 6.18x10^5 m/s, but I don't know how to proceed to part b)]
3) Consider a geosynchronous satellite with an orbital period of 24h. What speed must the satellite reach during launch to attain the geosunchronous orbit? (Assume all fuel is burned in a short period. Neglect air resistance.)
[On the ground, does the satellite have kinetic energy or is it at rest on the ground?]