What's really vexing to me is how spacex refuses to build a triple stage rocket. Their 'reusability' adds a significant amount of mass in terms of heatshield and in terms of fuel margins for landing. Using additional stages benefits them more than saturn V. They likely thought they could get away with two stages and have them both return to the launch site, one the short way, the other the long way around. But the exclusion of a multi stage reusable architecture means that their empty mass fraction becomes a linchpin in bringing anything into orbit.
No wonder there's a v2 and v3 with much, much larger fuel tanks and less payload.
No wonder there's a v2 and v3 with much, much larger fuel tanks and less payload.