"What would an updated Sea Dragon include?"<br /><br />Choices that make sense for a large sea-launched TSTO launch vehicle include:<br /><br />1) Non-cryogenic propellants.<br /><br />2) One type of engine, four of which propell the first stage and one of which with a larger exhaust bell propells the second stage.<br /><br /><br />The orginal conception of the SeaDragon described over at astronautix.com uses LOX/RP-1 in the first stage and LOX/LH2 in the second stage. If liquid hydrogen is troublesome to handle in ordinary circumstances just imagine the nightmare of dealing with it at sea! Even liquid oxygen can be difficult as SpaceX has discovered with the recent mishaps of the Falcon 1 rocket. Now imagine instead of the LOX boiloff problems SpaceX was having with the Falcon 1 rocket in a warm tropic breeze, the boiloff problems a SeaDragon would have with the LOX tank under the waterline!<br /><br />The propellant choice that would most simplify sea-launch handling issues is probably nitric acid/RP-1. This is much less efficient than the cryo propellants, but the SeaDragon isn't about efficiency, it's about brute size. If the rocket has to be larger to compensate for the lower performing propellants, so what. (I admit that cryogenic propellants would have to be used for any 'Earth-Departure' third-stage. But since the size of the third-stage should be much smaller and sit high out of the water, that eases the pain. Plus maybe a warmer cryo combo such as LOX/CH4 could substitute for the classic LOX/LH2 combo.)<br /><br />Using the same propellants for both stages simplifies and reduces development cost. Another reduction of development cost is by using a cluster of engines on the first stage which are the same as the single engine used on the second stage. That way only one type of engine and of a smaller size has to be developed. The original SeaDragon used one giant engine per stage but of two different types, each type of different size as well as of differen