I'd like to toss in a few observations regarding capsule versus lifting body proposals. If the CEV is going to be a core for several different missions, then that will have a big effect on the design. So will safety, as we simply cannot afford more crew losses like on the shuttles. The public and the politicians will not stand for it (and I'm sure the astronauts have views on that as well). <br />In which type does the consideration given to the re-entry and landing impact the least on the craft's other functions, for example, as a command module on a very long deep-space mission? <br />What shape best combines a strong hull (for when all hell breaks loose), with the ability to fly varied re-entry scenarios (from LEO or deep space), possibly with little or no crew control (because all hell broke loose)? Which one pulls G's in the same direction (relative to couch position) on both launch and re-entry, so that when an abort happens during boost and the poor sods are looking at a very hard ballistic trajectory, they are at least in the best position to ride it out, without having to try to move the couches? Which one could best survive being blown away from a launch vehicle while under severe aerodynamic loads, such as destroyed Challenger?<br />Which one can use an ablative heat shield, as opposed to a tile system (although perhaps new technology may come along to make the question moot)? <br />One of the things that pulled me away from wings and lifting bodies (although most capsules have some lift) is the rather hairy stories that have come out of the Soviet/Russian program. The most extreme case, aside from several aborts and ballistic re-entries, was when the equipment module did not seperate from the landing capsule after retro-fire. The two re-entered together; the back end finally disintegrated, and the landing capsule made it down. I wonder if any of the lifting body designs I've seen could survive that, especially on a return from deep space. Th