Ok, show me. DO the calculation. Give the correct amount for the payload.
Bob Clark
You claim, you prove. Ever heard of scientific method?
When you claim or assume something, you either prove it in your own paper as your own work, or you cite somebody. If you construct circular references like your infamous "Blog post A is correct because of blog post B, which is correct because of blog post A", yes, I pay attention to such details, don't be surprised if people are not convinced.
Also, your

question was, if a SpaceX Falcon 9 1.2 first stage can be used as expendable SSTO. Since not much data of a Falcon 9 is known to the public, I reconstructed a model of the Falcon 9 and then calculated the SSTO performance, and showed that it has only a subpercent payload mass ratio, which is a strong hint that more detailled calculations will not show a significant change. Also expending a 450 ton SSTO for the payload capacity of a much smaller and cheaper launcher (For example Epsilon) is sure not advancing mankind into space.
So, I had done more right now with just three hours of finding initial conditions, programming a genetic optimization algorithm and estimating the SSTO performance of the most suitable configuration, than you have done so far in the past months. You are highly in my debt now and demanding more from my side is only a sign of your dishonor and disrespect.
Also, what is the correct amount of payload? :lol:
I can of course do a second or third level calculation of the candidates. I can also include different engines and even largely risky technology like aerospikes. But that would mean far more work than just three hours of my life for a question, that is not mine. If the work will exceed 8 hours of my life, you won't find it here in the forum, but in a scientific journal that I can afford. :lol: