@K. Adams
"With a modest sacrifice in cargo capacity, you could add a parachute pack and an ablative cork outerliner (like what SpaceX is doing with its Falcon series),"
The capsule is called Dragon, Falcon is the launcher.
" and turn the pod into a reusable cargo module."
the key ablative is called PICAX, although their may be some cork used. Spacex seem keen on re-flying their capsules. Expdendable launch vehicle <> expendable capsule.
ESA have *talked* about enhancing the ATV design to act as a European capsule but has never got round to it.. The ARD programme demonstrated that Europe can do this.
"On the other hand, NASA's Space Shuttle, while reusable and very versatile, requires specialized refurbishment using high-tech ceramics and adhesives"
Reusable. Hardly. Refurbishable at best. The adhesive is "Room temperature vulcanisalbe" and is basically the stuff used to stick tiles to bathroom walls. But the tiles are specialized and expensive.
"Unless a good, reliable Single-Stage to Orbit (SSTO) technology comes along, I doubt we'll ever see anything like it launched again.)"
Depends what you mean by that.
"Like" as in wings? Possibly*. The cheapest *programme* option would be to go with a design which has lots of wind tunnel and flight experience IE the Orbiter shape. "Like" as in dump two refurbishable solid fuel boosters and an expendable propellant tank on the way up then I sincerely hope not. It would not be "Single Stage" would it?
As has been fairly well documented the STS was an architecture driven by a stupid funding pattern (which had *no* basis in the funding pattern of *real* large development projects), political coalition building and the technical failure of the engine manufacturers to deliver the spec they promised.
If you find the answer to the question is the STS architecture the *question* is FUBAR.
*Reaction Engines in the UK advocate a winged SSTO. Most SSTO supporters feel wings are a waste of mass and the cross range is unnecessary to the vehicles *primary* mission. The last serious attempt at a *preliminary* SSTO design was the DC-X with was large capsule shaped.
but planned to use a nose first entry (capsule cross range goes up quite a bit but so does heating).
Mines the one with the NASA Project Management handbook in the side pocket.