Everything has advantages and disadvantages.
Sure, at least the stuff we're discussing. If something has either all advantages or all disadvantages, we wouldn't have to talk about it...
With respect to 1) leak rates are nominally about 0.05% of cabin volume per day, so even over long missions the amount does not add up to much, although airlock purges will increase this significiantly.
I haven't seen the Shuttle or ISS figures, but on Apollo I was surprised at how much O
2 was budgeted for leakage, both from the pressure suits and from the cabins. It could be as much as or even more than the metabolic consumption. The actual figures were generally less than the nominal, but still nonzero. So unless seals have gotten a lot better, I wouldn't be surprised to see the mass loss rate on the ISS be considerably more because of its higher total pressure and the greater volume per crewmember. On the other hand, its larger size means more volume to surface area, which would proportionately reduce leakage rates.
2) indeed, although I don't have the numbers to hand, the percentage increase is small, I think and decreases proprotionally with larger volumes.
Sure, because for many shapes the volume increases faster than the surface area.
3) Indeed it is, as a diver I wonder if there is not excesive caution being shown with this.
I'm surprised to hear you say that. I keep hearing horror stories of divers experiencing decompression sickness sometimes even when they follow the standard tables.
DCS, fortunately mild, has definitely happened in space. Michael Collins wrote about his experience with it on his Gemini flight and how he was determined to avoid it on Apollo 11. He didn't report it at the time because he thought it would get him thrown off flight status. That's too bad, because it's a human physiology thing that can hit anyone, and you can allow for and prevent it if you know it's a problem.
I don't follow you, sorry. Russian EVA suits (principally the Orlan) have always operated at 400 mb pressure with pure O2, The US shuttle ISS suit (EMU) operates with only 296 mb of pure O2. The Apollo suit was even lowe, only 255 mb pure O2. They are all reduced pressure pure O2 suits.
Yes, but I wasn't talking about a fire hazard during the actual EVA but during the preparation. You're decompressing to suit operational pressure, and to speed it all up you're probably breathing O
2-enriched air (or pure O
2) to flush out the N
2 in your tissues more quickly.
The Apollo astronauts faced the same (fortunately theoretical) hazard when they prebreathed pure O
2 at 1atm or more in their suits starting at suit-up, through the walk-out and trip to the pad, and while waiting in the CM for launch.
This is more or less what is done on the ISS with the US suits, although the crews don't actually breath high pressure O2 in the suit, but wear masks beforehand.
Okay, that's probably the best approach as it limits the high pp-O
2 to just the mask and its supply hoses, and I presume they can be made oxygen-safe.
Orlan does not need a prebreathe, apparently
Why not? It uses pure oxygen too, right? The pressure might be a little higher than the American suits, but I can't imagine it's so high that DCS isn't an issue.