A rocket is fired vertically from the surface of the earth at a velocity of 5kms^-1. The acceleration of the rocket is given by a= -80000/x^2 kms^-2, where x is the distance of the rocket from the centre of the earth.
If the radius of the Earth is 6400km, find the rocket's velocity when it is 3600km above the Earth's surface.
So I integrated a to get v which is (v^2)/2=80000/x+c
HOW DO I FIND C ?!
If the radius of the Earth is 6400km, find the rocket's velocity when it is 3600km above the Earth's surface.
So I integrated a to get v which is (v^2)/2=80000/x+c
HOW DO I FIND C ?!