Okay, so I believe I a correct in that the plan is for this to release from the fourth stage at apogee, being pulled out by its own mass when the stage inverts and dangle nose down under chute.
if the only thing holding it in is gravity and acceleration on boast, I am wondering (and high power guys like
@Steve Shannon or
@JimJarvis50 might know.) whether transient decelerations during staging may cause drag separation of the tower prematurely. If this is NOT a possibility, ignore the following.
to keep the tower in place until the fourth stage ejection charge fires, drill a very small (1/8” would work) from the base of the attachment dowel/post, THROUGH the center of the nose to the forward end of the motor tube.
put a midline longitudinal hole in the center of your dowel/post heinie, and GLUE a needle in there so it sticks straight out maybe 1/4” to 1/2”. This is your micro “screw eye”. Emphasize it is NOT the shock cord attachment, it is not that strong, but it SHOULD be strong enough to prevent drag separation as the attachment point for a cotton thread. It should fit in the 1/8” hole easily.
during prep, run a piece of cotton thread through the eye of the needle, run both end down the 1/8” hole to the motor chamber, and run it out through the the motor tube.
when you are ready to put motor in stage 4, insert the tower in the fourth stage, pull the strings taut, and load the motor (the strings should fit between the motor and the tube.) Likely simple the friction alone will be sufficient to hold it in place, but as a belt and suspenders guy, you could do a couple wraps around the motor and tie a knot. Again, I’d think of thread the same way the high power guys think of those break away bolt thingies that keep the nose cone on until the ejection charge fires. Strong enough to maintain integrity during the boost part of the flight but NOT strong enough to function as a recovery system.
i leave up to you the true shock cord attachment for the tower itself.
at ejection, I am pretty confident that the ejection charge will burn the string and release the tower, which assuming a loose fit (graphite would help but is horrendously messy) the tower will slide out under its own weight (or drag separate, which is FINE at this phase of flight.)
I do NOT think the 1/8” hole will significantly decompress the motor tube, so again assuming a loose fit for your rear deployment system, I don’t think this will compromise it.
not sure if this is not the most complex non-electronic rocket ever (especially since
@JAL3 never completed the Rube Goldberg Lander, mores the pity!
), but definitely one that would benefit from a preflight and launch checklist. I have encountered fecal turbine interaction on much simpler rockets where a checklist would have saved the day.