I recently read is some article (can't remember which one for what its worth), that you could damage either the O ring(s) or the housing itself be flying with it shut since there would be "negative pressure" on it.
Since most airliners are perssurized to 8000' this would be where the atmostphere is 11 PSI which is a 3.7 PSI differential from where I would seal it up at sea level.
Since my housing is rated to 130', taking it to this depth on the other hand would mean a PSI differential of 58 "positive pressure"
(130/33+1=4.93 atm * 14.7 = 72.6 PSI -14.7 = 58 PSI differential)
So does having a "negative pressure" of 3.7 PSI at 8000ft altitude really hurt the O ring and/or housing more than a "positive pressure" of 58 PSI does by having it at 130' underwater???
Thanks!!
Since most airliners are perssurized to 8000' this would be where the atmostphere is 11 PSI which is a 3.7 PSI differential from where I would seal it up at sea level.
Since my housing is rated to 130', taking it to this depth on the other hand would mean a PSI differential of 58 "positive pressure"
(130/33+1=4.93 atm * 14.7 = 72.6 PSI -14.7 = 58 PSI differential)
So does having a "negative pressure" of 3.7 PSI at 8000ft altitude really hurt the O ring and/or housing more than a "positive pressure" of 58 PSI does by having it at 130' underwater???
Thanks!!