Thinking a bit more to your problem, I seem to recall now that in the fabrication of rocket sections, with say 5 m diameter and thickness of may be 5 mm, they stabilize them during fabrication by a small gas pressure. However this has nothing to do with column instability, it is used to avoid local instabilities due to local loads caused by handling.
Column buckling is due to the following phenomenon. When the column starts to buckle, the deflection will have two effects: one is the elastic energy due to
bending stored in the bar, the other one is the shortening of the column again due solely to the
bending deformation, that will need a work to be done by the load.
When the elastic energy equals the work done, then the instabilty occurs.
As you see the axial stress in the column, contrary to what one would expect, has no role to play, that's why I think that the buckling load is independent of the internal pressure (or possibly with a very low dependency due to secondary phenomena).
If the buckling could be caused or initiated by a local instability, then the internal pressure would help in avoiding that. However this would be true particularly for thin cylinders, but I don't think you have a very thin one with that pressure.
However all the above is true for the so called elastic instability. When the plastic one is controlling (and I recall now that you mentioned a short cylinder), then you could be on the right path, as the plasticization of the section under the axial compressive load will not start, until the axial stress due to pressure has been overcome (provided your pipe is end capped).
However I'm not able at the moment to provide definite design suggestions for this. Of course you should account for a loss of pressure when an axial load is still acting. Also you should check that local yielding does not occur where the stress due to pressure is not present (cylinder ends).
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