(presuming we are talking about nominal positive or negative deltas either way of say no more than about 12 or 15 psi or so)
I'll assume that the 12-15
PSI you mentioned was a typo and that you actually meant 12-15
inches of mercury- which is representative of engine vacuum.
Perhaps GM does have a technical paper on what would happen if a vacuum system inadvertantely becomes pressurised, but I would be truly surprised. I'm sure they spent their R&D dollars on more productive efforts.
I made the comment about it potentially damaging the system as some newbie may follow bad advice and pressurise it with 12-15 PSI- or whatever a shop compressor can muster.
When restoring my car years ago, I used a laboratory grade vacuum/pressure combination pump with a relief valve set at 15 in/hg. Initially this was set to 'vacuum' and connected to the system inlet tube on the intake manifold. I was unable to find many leaks as the noise of the pump drowned out the subtle 'hiss' from the leaky components. I reset the pump to 'pressure' and repeated the test, thinking that I might 'feel the breeze' from whatever was leaking. Immediately upon starting up the pump, both headlights slammed closed- the opposite of what was commanded by the headlight switch.Why? The system was operating in reverse.
I shut off the pump and set it to 'vacuum' again, expecting both headlights to raise as commanded. Nothing. Long story short, the front seal on one actuator had been dislodged from it's mount creating a huge leak to atmosphere and was now preventing the system from building any meaningful vacuum.
Dis-assembly of the actuator to replaced the dislodged seal (commonly called a witches hat) showed a design which was obviously meant to have pressure in one direction only. Had the seal not been dislodged from it's seat- ending the experiment, continued use of pressure on the front side of the actuator would have resulted in leakage around the seal/actuator rod interface. This 'leakage' would have given a false indication of a defective seal- when in actual fact it was simply been subjected to an operational configuration it was not designed for.
The comparison with the brake piston seals (common to the the aircraft engine trade as well as automotive, and known as a 'V' seal or 'Garlock' seal) is valid for similar reasons. The source of air entering the hydraulic system at thew caliper end is most often from piston 'knock back' where there is momentary reversal of pressure across the seal.
In the aviation field, the value of .5 psi is considered the maximum allowable pressure reversal as a design limit.
I hope you can see and accept the correlation