Cabin Pressure question
I recently discovered that the STS Orbiter (and therefore the ISS) was built to hold a cabin pressure of 14.5 PSI near sea level conditions. I had previously assumed that the shuttle was built with the 8 PSI differential that most jet airliners are designed for.
This change must have added a lot of weight to the orbiter. Structure, particularly the windows all had to be strengthened considerably for that extra air pressure. This seems to be a costly design choice in such a weight critical spacecraft. While sea level air pressure is a big advantage, especially for a normal 78/21/1 atmosphere, I wonder why they couldn't get by with a lower pressure/higher cabin altitude.
We do just fine flying airplanes breathing basically 8000 ft earth air, why do much more fit astronauts need sea level air at the expense of probably a couple tons of launch weight.