A space station has a radius of 200 meters. An astronaut has a mass of 55 kilograms and the station rotates at 1.5 rev/min. What is the period of rotation for the station?
The Attempt at a Solution
I think the FNET equation is Fsp=ma and I'm pretty sure you have to solve for [tex]\tau[/tex] but in order to do that I need to solve for a. How do I either find a velocity or acceleration to do this?