An astronaut weighs 1000N at the surface of the Earth of radius 6500 km, what his weight will be at 13000 km and 19500km from the centre of the earth?
Do I have to calculate the new value of g at 13000 km using the following?
(G• Mearth) / (Rearth)2
Where:
G = 6.673 x 10-11 N m2/kg2...