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> Best reliability calls for a completely reuseable single stage launcher Alas, SSTO fuel fraction is prohibitive. 2STO typically uses 1/3 the propellant for a given payload, although vehicle empty weights are higher. > separating two vehicles at high speed in the atmosphere is not simple. Shuttle does it every mission - SRBs from ET, ET from Orbiter. > Series staging is terrible because you take off without the second stage engines > running, and thus without knowing whether they will start and run correctly. Agreed > In any case there's little reason to use multiple different engine designs in one > vehicle. Servicing a single engine type is cheaper, if all other things are equal. 4 on the booster and 1 on the Orbiter would support a single engine core, with differing bell arrangements.
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