Earlier quoted context omitted.
> This is generally (but not always) false. SpaceX has been negotiating a lot of their commercial contracts in a vehicle agnostic fashion. Here's another way of putting that: SpaceX has designed it so F9 and Starship payloads will be interchangeable. That's not quite the same thing. You can't just take an F9 payload and bolt it on top of an Ariane rocket. > Starship is being designed with the intent that it will cann…
I find that utterly mad why would you combine multiple small launches into a big one? The tyranny of rocket equation suggests to me that you will have to burn a lot more to lift a lot more things to burn for the payloads that would have been in a different rocket. I would like to be shown the math that it actually takes less fuel with a bigger rocket.
Reusability is a spectrum. Falcon requires a nontrivial amount of inspection and refurb between launches, while Starship is aiming for jetliner levels of prep.
Musk is also aiming to drive down the capex costs as well. There's less complexity for unmanned cargo hoist missions. I think the target for Starship is low tens of millions USD, basically cheaper than Falcon Heavy, but more reusable, with more capacity.
I think the only thing that's not cheaper, is liquid methane is a bit more expensive per kJ. They are roughly the same price per kg, with RP-1 being more energy dense. But then again, I could see SpaceX vertically integrating and driving that cost down too.