Arturo O. answered 12/18/19
Experienced Physics Teacher for Physics Tutoring
(a)
vB = √(GM/R) = v
Note the speed depends only on the radius of the orbit and the mass of the planet, but not on the mass of the satellite.
(b)
vB = √[G(2M)/R] = √2 √(GM/R) = √2 v
(c)
2v = √(GM/RB) ⇒
RB = GM / (4v2) = GM / [4(GM/R)] = R/4
(d)
vB = √[GM / (2R)] = (1/√2) v
(e)
Use Kepler's 3rd law.
RB3 / TB2 = RA3 / TA2 = R3 / TA2
RB3 / (8TA)2 = R3 / TA2
RB3 / 64 = R3
RB = 4R