Re: Meanwhile over in Ars Technica...
>Apollo rockets used hydrocarbon (~kero.) and liq. oxygen while the second stage used liq. oxygen and liq. hydrogen
LH2+LO2 gives best bang / weight, so you use it for second stage where you have to lift all the fuel before you use it. But if you need a really BFR the cryo-tanks get really-really big, so you use Aga-fuel+LO2 for the first stage.
Think of it as methanol powered Nascar vs Diesel Tonka truck
>(or why the shuttle required solid fuel boosters)
Fuck, I've run the numbers and these insanely complex cryo engines we reused from the Saturn V 2nd stage aren't going to move the Shuttle. We are going to need some serious help(*)
(* 1st rule of explosives, if it doesn't work - add more explosive)
> the practicalities of handling cryogenic liquids
Don't tuck your trousers into your boots and make sure your fly is done up.