Come dyno day, we'll see if indeed I might have too much lift.
I'm really pleased to see you showing an interest in this build, I'm sure that this engine is going to be a good step better for it.
I stopped playing with A series engines before I got into the habit of plotting every cam that came my way, so can't help with your valve accelerations, but I suspect it'll be the maximum you can get from the follower diameter. I can't disagree with your comments about inlet valve closing time (I don't have anything like your knowledge on this), but I was coming at the 1.25 rockers from a different direction, that of reducing overlap (measure that how you prefer). To me the magic happens during overlap, and equally it's the phase where things go wrong if you don't have the acoustics right. It's unlikely that this engine will have the right lengths and diameters without a lot of dyno time, so mine was a suggestion that less may be more. I'm a simple soul, and like to keep my theories simple 
With regard to optimising inlet valve closing time and compression ratio; will that still be correct in the ~85% atmosphere at 4000ft? I have no experience of this as 400ft is high around here, but I suspect that an engine that's fussy in this respect will struggle at Bonneville. I throw this out there as I'm interested in the answer.
go fast
Andy
Thanks for the confidence factor. I also suspect that the flank accelerations of this camshaft are @ or near the maximum for the follower diameter. Whether that is good or not depends mainly on whether the valve is open enough, Vs TOO MUCH, for the port to be able to flow enough to meet the peak demands of the cylinder ATDC, @ SOME SENSIBLE GAS SPEED. This can be calculated and I've started doing some of these, but I am hung up @ the moment from lack of dimensions/airflow numbers of cyl head/exact cam profile/etc, etc. Pipe sizes and lengths can be calculated & modeled, & again I need more information about other engine build specs. Yes, it can be done with LOTS of dyno testing, but that is expensive and will use up a "test mule". My experience is that modeling & simulations can save time & cut cost, AS LONG AS THE CONCLUSIONS ARE CONFIRMED ON THE DYNO. I have some good experience doing this, on both BMC & Ford/Lotus/Cosworth 4 cyl engines, and trust me, going to the trouble of figuring things out ahead of time is the way to go. No more cut & try for Fordboy!!
I am going to presume that by acoustics you are talking about wave tuning of the inlet/exhaust systems. In terms of valve events, the effective inlet closing point is the most important, because it directly impacts DYNAMIC compression ratio. Your STATIC compression ratio is what you calculate in terms of displacement differential, but your running engine doesn't care about that. And even if your static C/R is 13/1, if your volumetric efficiency is 110%, then 13x110% = 14.3/1 at that V/E!! You might want to know that, if only for the additional stresses on the parts. However, no BMC I ever dynoed made over about 90/95% V/E, because of the 5 port head. Now some BMC's don't get to 90% V/E, because with their limited airflow, they are sensitive to "build combinations". Your decision to be conservative on parts is a sensible one, because as the output is raised the engine becomes more "sensitive" to parts combinations, AND, there are MORE OPPORTUNITIES TO BE WRONG. Think about that, like I said, it's complicated. Now I want to qualify my experience with BMC's and defer to those with more & longer experience in building race combinations, some have probably exceeded 100% V/E, I just don't know about them. But back to the example 13/1 C/R @ 90% V/E = 11.7/1 C/R. Hence, my issue with wanting to know the BMEP of this particular BMC engine combination. Peak BMEP of well thrashed combos SHOULD be around 220/225psi. Lower numbers indicate room for improvement, REGARDLESS of where the improvement comes from.
Valve events at overlap present some opportunities for impressive wave tuning or massive reversion. In any racing engine, the returning exhaust pressure wave can & does create inlet tract pulses that exceed peak cylinder demand EARLIER than peak cylinder demand is typically encountered @75/80 degrees ATDC. The trick is to tune the combination to take maximum advantage of this. Again, simulations & modeling can help here. Reducing the overlap, anyway you can, helps alleviate a bad reversion condition. On hot street/street engines, prevention of reversion should be the focus.
There will be some small effect from the thinner atmosphere of high altitude, mostly lessening the V/E of the engine, perhaps some effects on the gas speeds. That is why lots of land speed vehicles are blown or turboed. But if you are running naturally aspirated, the air is the air, and you can't do much about it, EXCEPT, plan for it, AND, take advantage of the lower V/E. Rejetting the carb will be essential. Static C/R will of course, remain the same, regardless of altitude. BUT, Dynamic C/R can be manipulated to take advantage of the lowered V/E. 85% density x 90% V/E x 13/1 C/R = 9.945/1...................

Stay tuned, I intend to model this. Whether Midget's engine can take advantage of any changes the modeling suggests, remains to be seen. However, I believe that right now, there is room to improve engine performance significantly, and have an engine that will work in Utah & North Carolina. Like I said, stay tuned........
Best regards &

MB