| 17. |
Neglecting air resistance and the weight of the propellant, determine the work done in propelling a 6-ton satellite to a height of
(i) 300 miles above Earth
(ii) 400 miles above Earth
Assume that Earth has a radius of 4000 miles.
| A. |
(i) 1,004.65 mi  ton; (ii) 1,309.09 mi  ton |
| B. |
(i) 2,511.63 mi  ton; (ii) 3,272.73 mi  ton |
| C. |
(i) 1,339.53 mi  ton; (ii) 1,745.45 mi  ton |
| D. |
(i) 1,674.42 mi  ton; (ii) 2,181.82 mi  ton |
|