The aircraft has been test flown with a fixed pitch 62" X 93" Prince P-Tip prop.
The performance figures we have achieved so far are as follows:
Static rpm (1013hpa/30degc day) is 4800rpm.
Initial climb at 120ktas gives 5000rpm and 1100fpm.
Straight and level figures at a density altitude of 4500' are as follows:
5500rpm - 175ktas
5800rpm - 181ktas
6000rpm (tested once for a short duration) - 184ktas.
The engine was at nowhere near WOT at 6000rpm.
So, we clearly need more top end pitch and less bottom end pitch, i.e. an IFA prop.
I have contacted the usual suspects (Airmaster, Woodcomp, Ivoprop, Variprop etc.) but with a limiting prop diameter of 62" (maybe 64" at a pinch) the IFA prop manufacturers struggle a bit for a blade that will suit the slow turning, small diameter high speed application.
We may need to consider a custom blade to suit one of the hubs.
Before we go to that extent, does anyone have any suggestions for this application? I my well have overlooked options.