Whatever you decide I suggest you contact the TRA class three committee before you start construction.
A three stage with P motors may stretch the waiver radius.
M
Yes!
This is what is making me lean more toward a two-stage heavier rocket. Given Jim Jarvis's comments on the subject in his multistage rocket thread, I'm entering with caution. I happened to be one of his other beta testers for stabilization hardware, so his commentary on the subject holds a lot of weight for me. The good news is I have the software, and skills to do much of the testing and analysis before ever submitting anything to the committee.
The one hangup I have is the simultaneous ignition of two P-motors, as well as their simultaneous burnout. Any major thrust variation on either end could dramatically alter the launch profile - at least in simulations. Has anyone had a good solution for this besides stabilization, or thrust vectoring? From a safety perspective, I don't want to require either for this to be successful, that's a fools errand. Just want good video.