Could someone please provide good data about the Hercules' power at altitude? The data I have is from the chart found at the AEHS site (cca 1390 Hp at 5100 ft, and 1220 HP at 13000ft, all while using +6 lbs/sq in at unknown RPM); at 20000 ft the chart gives 900 HP.
The entry at WIlliams' site mentions the +8 lbs/sq in at 2900 rpm, the full throttle height with ram effect being 8,500 ft (327,5 mph) and 15,600 (333,5 mph); at climb the boost was restricted to +6.
The entry at WIlliams' site mentions the +8 lbs/sq in at 2900 rpm, the full throttle height with ram effect being 8,500 ft (327,5 mph) and 15,600 (333,5 mph); at climb the boost was restricted to +6.