Here's a snippet of the launch, plus a couple of stills. I lost it on the screen after this point.
Some pretty major fishtailing going on, altho doesn't seem actually unstable.
I would like to index it versus the thrust curve to see where the BP peak thrust was. Because stability is only produced when the inductive gas velocity is high compared to absolute (model thru air) velocity, i have an idea that if acceleration during the peak thrust is sufficient that the induction/air velocity ratio during plateau thrust is low then stability is lost, or at least becomes marginal. This would likely be very early in the flight for this motor, possibly before it cleared the rod.
Next test is to try a motor with a longer and pref flatter thrust profile, like A3 or better B2. These should show more clearly what is happening with stability.
I am also going to compare the model parameters more closely to the stability conditions in PoF379, my guess is these may be marginal due to the difficulty in getting the motor far enough forward within the scale geometry, but this would be much better for a model at 3-4 times this size.
I also plan to add a small internal launch lug (at the moment it has none at all) to give it a truer lift off - I can't be certain it didn't ever so slightly snag on this test, which could be another contributor to fishtailing.
The model tumbled to ground before ejection but with no damage and no sign of any burn to the induction tube, the motor load/reload section was easy plus the GDS ignition method worked well for the second time.
Overall these points seem tentatively promising for a scale up.
View attachment TRIM_20220312_191809.mp4
