Instant Shuttle turnaround ?



This is a rethorical question, so no need to spout insults about how
unrealistic, unsafe it would be. I am more interested in the raw
mechanics of it. (and a "one off" exploit, not doing the stuff below all
the time).

If, just after landing, they were to clean up the cabin, refuel the
tanks, inflate tires and then mate an orbiter to a stack and launch it.

What orbiter systems would not work because they *absolutely* need to be
changed with each flight ?

What systems would have a high likelyhood of failure ?

What systems would likely work ?

What systems would definitely work ?


Would it be fair to state that the cabin systems, computers etc would
not *require* any refit between flights ? (ok, so they need to change
the CO2 filters and clean toilet).

Would SSMEs work ? Or do they become absolutely inoperative after being
iddle in vaccum and/or re-entry ? Is it correct to state that they were
originally designed to be re-used without maintenance ?

What about all the thrusters around the orbiter ? Do they gunk up during
re-entry and require maintenance, or are they theoretically ready to be
used again ?

.



Relevant Pages

  • Re: Instant Shuttle turnaround ?
    ... What orbiter systems would not work because they *absolutely* need to be ... changed with each flight? ... re-entry and require maintenance, or are they theoretically ready to be ...
    (sci.space.shuttle)
  • Re: Instant Shuttle turnaround ?
    ... What orbiter systems would not work because they *absolutely* need to be ... re-entry and require maintenance, or are they theoretically ready to be ... main engines were originally designed for complete rebuild after each ... flight, they have a high ISP nand run right on the edge. ...
    (sci.space.shuttle)
  • Re: Space Shuttle Drag Coefficient
    ... Reunite Gondwanaland (Mary Shafer) wrote: ... Dryden web site and search the DTRS, you'll get a much better copy. ... Orbiter Flight Data", Iliff and Shafer, TM X-4500, June 1993, ... Space Shuttle Orbiter During Reentry Flight ...
    (sci.space.shuttle)
  • Re: Obvious solution to the "foam problem"
    ... payloads implemented by the safety assessments of the orbiters original ... the sts-107 orbiter stack particularly vulnerable to the wind shear ... enhanced flight profile through the region of high dynamic pressure. ... enhancements in attempting to make the shuttle fleet as operational ...
    (sci.space.shuttle)
  • Foam damage throughout history
    ... An article in Aviation Week about STS-2 noted that foam probably struck ... the orbiter on that flight, and there was tile damage. ...
    (sci.space.shuttle)