1. The problem statement, all variables and given/known data A 300 kg rocket sits on a launch pad. What is the thrust needed to obtain a thrust to weight ratio 3:1? 2. Relevant equations 3. The attempt at a solution 300.0 kg x 9.817 m/s2 = 2945.1 N i know this is not the correct answer, but i have no idea where to start. can someone please help?