Keith:
> Uh, I think you're missing something here -- there's no change in any
> acceleration values across apogee; the rocket trajectory is ballistic
> precisely because the only large force acting on it is gravity, which is
> constant.
Your're right.  :-)   I really don't understand what the accelerometers are 
reporting. I assumed that the accel would detect the de-acceleration as the 
rocket reached apogee, reach a point of zero acceleration and then start 
accelerating back toward Earth.  In retrospect, this is the vertical velocity 
vector. Since it is a vector and the rocket is pitching over the calculation 
requires some interpretation of the direction that the rocket is pointing.  If 
the software is not integrating the direction of rocket, how do you estimate 
apogee by acceleration alone?
Craig 
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