Maybe try making the wings a bit thicker so you don't lose much on scale looks but get a lower stall speed?
It's great to hear she flew well!
Have you thought about a bungee launch system to help with keeping that initial speed high and thumbs on the sticks?
Thanks for the recommendations. I have looked at both of those possibilities.
In terms of making the wings thicker, I used a Clark Y airfoil on version 1. It has an excellent lift coefficient and a very gentle stall character. There are higher lift airfoils out there, but going to a much higher lift airfoil would either mean incurring a significant drag penalty, or using an under cambered airfoil which would make inverted flight a pain. I've attached the airfoil profile and lift curve for the Clark Y airfoil I initially used from Airfoil Tools.
As can be seen, version 1 used a pretty thick airfoil already. I'm actually going to a thinner lower lift airfoil for version 2. Having a larger design that can accommodate retracts and flaps means I can increase the lift coefficient well beyond what could be achieved with a flat bottom airfoil by dropping the flaps while simultaneously meaning I have to worry less about takeoff speed. Mixing in maneuvering flaps should also improve turn rate. The better L/D ratio should enable a better top speed as well. Because of the location of the horizontal stabilizer, a stall angle beyond about 10 degrees isn't too useful. The wing can blank out the stabilizer and result in a deep stall. With the Clark Y airfoil, I had to be very careful to avoid that, but with the new AG37 and AG35 airfoils, it should be much more difficult to put the airplane at a high enough angle of attack to get into that situation.
To avoid tip stalls, the airfoil at the wing root is different from the airfoil at the wing tip. When the airfoil is the same throughout, as it was on the version 1, the spanwise flow and lower Reynolds number at the tip means the tip stalls first. If one wing tip stalls before the other, the asymmetric lift results in a tip stall. The easiest way to avoid this is with wash in the wingtip, but it's hard to get that precise without a complicated jig. The change in airfoil from root to tip results in a bit more drag since the lift distribution is a bit less ideal, but it makes the construction process much simpler, and the increase in drag is pretty tiny.
In terms of a bungee launch system, that would have been ideal for version 1. I actually went as far as measuring out lengths on some spare PVC pipes, but the goal of the smaller plane was ease of transport. Moving the bungee launcher and plane is harder than moving the somewhat larger 64mm plane by itself, so I'm just increasing the size of the plane since I already had a spare 64mm fan, and otherwise the electronics are identical. Landing gear was always the goal and version 1 was just too small to accommodate reliable servo driven retracts due to their weight.