| 4. |
Neglecting air resistance and the weight of the propellant, determine the work done in propelling a 10-ton satellite to a height of
(i) 150 miles above Earth
(ii) 350 miles above Earth
Assume that Earth has a radius of 4000 miles.
| A. |
(i) 867.47 mi  ton; (ii) 1,931.03 mi  ton |
| B. |
(i) 2,168.67 mi  ton; (ii) 4,827.59 mi  ton |
| C. |
(i) 1,156.63 mi  ton; (ii) 2,574.71 mi  ton |
| D. |
(i) 1,445.78 mi  ton; (ii) 3,218.39 mi  ton |
|