Hi wxrocks.
Meaning, wouldn't the o-ring lose more "heat" through evaporation of the material itself and blackbody radiation.
There is no evaporation that might result in a heat flux, nor any significant evaporation at all. Nitrile O-rings are used for vacuum systems all the time, and long before you'd see any significant heat transfer due to evaporation, you'd see a sharp rise in the vacuum pressure but that doesn't happen. Nitrile is perfectly acceptable to use in a hard vacuum.
Regarding blackbody radiation, an O-ring should be completely enclosed by some metal gland, so the O-ring itself doesn't see significant radiation heat transfer, it's the metal parts around it that do. That said, your other parts shouldn't be any colder than the environment. If in a vacuum, the temperature will still come to some thermal equilibrium through radiation heat transfer.
I know CO2 is corrosive under pressure, but I want to eliminate any other sources of this corrosion in my system.
Looking in a chemical resistance guide for elastomers, I see nitrile is the proper material for sealing CO2, it won't be attacked, even with wet CO2. CO2 shouldn't be corrosive under pressure, but if CO2 comes into contact with water it can create an acid. Nevertheless, nitrile is still compatible and won't be attacked by that.
- What metal is the nitrile and CO2 in contact with?
This may be a shot in the dark, but could there be a radiation component to this problem? Perhaps repeated use in planes, etc. is exposing it to high energy radiation -- thus causing a breakdown?
Checking material compatibility again for nitrile versus radiation (ie: nuclear radiation) I see nitrile is rated BC which is not great, but not catastrophic either, and that's for very heavy nuclear radiation as might be exposed in a nuclear power plant. So to answer the question, nitrile shouldn't be significantly affected by high altitude (ie: aircraft) radiation.
- What are the symptoms you're seeing in the O-ring? What conditions is it exposed to (ie: altitude, temperature, CO2 pressure, etc...)? What is the extrusion gap (ie: the gap the O-ring would extrude through if it were a fluid)?