1. The problem statement, all variables and given/known data If ashuttle has a centripedal accelerationof .54m/s2, what is the weight of a 50kg astronat in that shuttle? other info I don't know if I need. T= 5400sec r=400,000m 2. Relevant equations fnet = ma I don't know if I am supposed to use [tex]\varpi[/tex]= mg + ma but I don't think so 3. The attempt at a solution so basically I'm just verifying if I should do f = ma and that will give me the weightofthe astronatu? thanks.