Did some maths about Super Heavy and Starship. Wanted to know how much delta-v that thing had, with zero payload - and then how "far" could it go with or without LEO refueling.
Well, say what you want of Musk, but the goddam thing truly has jaw dropping performance.
Super Heavy has a 0.95 prop mass fraction, which is nothing short of astonishing. Then again, Atlas made of steel - balloon tanks - and Titan II stage 1 were in the same ballpark.
Starship is a bit lower, 0.923 but that's still quite good, on par with Saturn S-II and better than a S-IVB. Which used LH2, to their credit.
The whole thing stacked fueled fired, with zero payload and no refueling in LEO would have a total delta-v of 14 000 m/s. Not enough for 9400+3100+2400 that is, Earth surface to Moon surface one-way trip: that would be 14900 m/s. Well, that's why it refuels in LEO.
Still, 14 000 m/s is plenty enough for 9400+3100 = 12500 m/s to a TLI... and that, with 50 mt of payload. Enough to carry and drop Apollo CSM+LM (45 mt together).
I also get 200 mt to 9600 m/s, which is plenty enough for LEO. Six flights like this would lift 1200 mt of methalox, enough to refuel a Starship and send it to TMI : Trans Mars Injection.
That thing is a beast of a rocket, for sure.