
Arturo O. answered 05/20/16
Tutor
5.0
(66)
Experienced Physics Teacher for Physics Tutoring
Use total energy equation:
KE + PE = (1/2) mv^2 - GMm/r, where m = mass of spacecraft, M = mass of planet, r = distance from spacecraft to center of planet
To find minimum velocity to escape from the surface of the planet, set KE+PE = 0, r = radius of planet = R
Note m cancels out, i.e. the answer does not depend on the mass of the spacecraft.
(1/2) v^2 - GM/R = 0
v = sqrt(2GM/R) = sqrt[2 * (6.67 x 10^-11) * (1.54 x 10^23) / 2.64 x 10^6)] m/s = 2.79 x 10^3 m/s = 2.79 km/s
Note answer is of the order of a few km/s, which is a typical planetary escape velocity.