To clarify a few things, my guess is that the AUW of this plane is going to be 14 pounds with 2x 4400 6S batts, plus whatever the wing extensions are. Let’s say 14.25 lbs, 14.32 with a CF 23x9 Falcon prop option, and let’s estimate that the 85 inch wingspan comes out to a 1290 sq-in wing area. That’s a wing cube loading just under 9, which is what we are all flying right now on the 78 and the 91 Extras. So, perfect, IMO.
Either of the two prop option will still produce a 2-to-1 thrust-to-weight, 270 to 290 Watts per pound, with a 6 minute flight time, at a 26 oz/sq-ft wing loading.
98A with a 4400mAh capacity:
98A / 4.4Ah = 22.3C
60 minutes / 22.3C = 2.69 mins at WOT
2.69 mins x 0.8 safe capacity = 2.16 mins at WOT
~35% power average (2.16/.35) = ~6.2 minutes
Everyone's power average is different but this seems to be the value with most of the contributors on the power thread. Tom's about a .44 so he would need 5300mAh for 6 mins, which would add 180g or 0.4 pounds, which would screw everything up. :sadface:
I’d try both props to see which one gives me the best blend of throttle response, pull-out, and top-end speed and go with it. I’m fairly sure this will be a really fun plane if the AUW is real, and even better if I've overestimated.
The other option is to go with the lighter motors and 3300's and bring this plane in at 12.7 pounds, probably, but it will be a very busy motor at about 220 to 230 Watts per pound on an 85 inch wing. You'll be spinning a decent 21 inch beechwood or CF prop max because the 22's do load these A60 and DM4330 systems a bit too much (IMO). I would be curious to see what a WL of 23 and WCL of just under 8 would be like at 1.7-to-1 thrust to weight tho. Probably nice and floatie, but not very dynamic.