I still don't understand the point of your comment then. Yes, the rocket's (potential) TWR will be above 1 at all points of the flight. What does that have to

I still don't understand the point of your comment then. Yes, the rocket's (potential) TWR will be above 1 at all points of the flight. What does that have to do with the comment you're replying to? The Falcon 9 has 9 engines. The combined thrust of all of them has to be greater than the weight of the fully loaded rocket. That doesn't mean a single engine will always have more thrust than the weight of the entire rocket.