The 109G6 performance graph was not presented prior. I do stand corrected on that count, though no data other than Xavier's assertion for 109G6/AS performance is presented, which is undoubtedly slightly better with the larger DB603 supercharger installed on the AS variants. I am surprised the G6 drops off so much above 22k, regardless, why would anyone fly a 109G6/AS with a 30mm over a K-4 with a 30mm which will fly 425 mph at 28k? Definitly have to keep that in mind for all those 30k dogfights.
What is the physical difference, sources sayit looks identical to the G-10. Is this for a MW, I have not been able to find any production #s for any AS variants, start a thread~ interesting but no less redundant.
Btw Karnak, the 47's Turbocharger achieved max rpms of 18,250 at 23,000 feet and remained constant through 35k though horsepower/manifold pressure is gradually lost at higher altitudes.
Altitude Turbo rpms rate of climb
15,000 14,050 2330
20,000 16,450 2150
23,400 18,250 2000
25,000 18,250 1810
30,000 18,250 1190
35,000 18,250 570