Ken, here's the result of doing the math in reverse that I tech-talked today,
PSI = 66
CR = 3.375 : 1
that's below the CR of 4.7 that someone quoted for the Model T,
but is around the CR for model turbo-jet engines that have been used in some RC planes (it should be noted that the exhaust gas temp for model jet engines is in the 500 to 600 Celsius range, and that's with mixing in lots of cool compressor air in with the combustion gas before turning the turbine).
so its not that an engine with this low compression cannot run, rather that its exhaust will necessarily be hotter (the lower the CR the less mechanical energy you're extracting from the combustion energy, leaving it hotter).
rather it would be helpful to know what PSI is observed in other running Atkinson Differential engines to see if you're in the right ballpark, using similar measurement gage, similar volume of pipes and fittings, and especially similar one-way valve, as these things will always introduce errors so best to compare by using the same errors
!
my guess is that 66 PSI / 3.375 CR is too low, and it should be up above 100 PSI where folks that have measured their run-able engines seem to get (they're not seeing the theoretical 166 PSI for 6:1 CR because of "pumping losses", IE valve timing and manifold vacuum issues, plus heat lost through the head and cylinder walls, all of which is expected).
for the A-D engine I suspect that valve timing is an issue in addition to head room. if the valve timing is built into cylinder ports like in a 2-cycle model airplane engine then there's not much to be done except make a new one (unless its also a function of the weird crank pins and rods that I vaguely remember, or maybe the A-D doesn't have as weird a mechanism as the A-C engine does ?), but the head room might be easier to adjust and experiment with ???
I guess the good news is that getting 66 PSI means your rings are sealing, although that might still improve with more break-in.
Peter.