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Interesting. I was under the impression the two seat Il-2 supplanted the single seater on the production line, but from what you're saying the single seater continued to be produced alongside the two seater. I'll have to discuss the best way to handle that with the mod team.
Would you happen to have any sources on the take off power of the Klimov M-105(R?) and M-105RA used on early production Pe-2s? I've found some data online but its a bit contradictory and I'm suspicious that some of the sources may be mixing up different variants of the engine.
I have to ask, though - with a nick of "Darth Tabby", are you 501st?
Ok.. the Klimove M-105 engine ... In 1940 Klimove designed М-105 engine of 1100KM power for taking off. The power at the ground level was 1020KM. And this info is the basic one. In 1940 the engine was introduced into production for both fighters and bombers. The unit for fighters was marked as М-105П while the one for bombers М-105Р. The letter "П" means "Пушечный" - for a gun because there was a possibility of mounting a gun at the engine block and firing through the reductor device. The letter "P" means "Pедукторный" - with a governor for a prop. But all the engine data for them was the same as for the M-105 In 1941 the engine was modified mainly by improving and reinforcement of its construction . The variants for a figter and bomber were marked as М-105ПА and М-105PА. The power for the variants of the engine was still at the same level. Here is a shot of a chart from H.W.Sorokin's book titled " История конструкций авиационных двигателей в России и СССР" - The history of construction of aviation engines in the USSR. The first line is the max power at the ground level. The second one is the nominal power at the ground level. The third line is the nominal power above the ground with the first speed. The fourth line is with the altitude for the first speed. And the fifth line is with the nominal power at the altitude with the second speed. So the entire mess with the power data seems to be caused by the using of the data for different altitudes (levels) it was measured.
View attachment 626745
the pic source: Авиационный двигатель М-105.
... Thanks, that's really helps clear things up. I think some of my uncertainty came from one source that suggested the ПA was optimized for lower altitudes but I think said source may have gotten it mixed up with a later variant of the П series M-105.
Also for some reason most English sources seem to refer to the "P" engines as "R" engines and the "П" engines as "P" engines.
Anyway thank you very much for the help.
380/381 were merged as 381, 381 changed to La-5 and moved to Moscow in early 43
could not find a 240 associated with IL-2 production
Ahh...ok, was just wondering.
I'm with Stormtrooper Ranch and occasionally troop alongside 501st at events.
I'm a TIE Pilot as well as a Tank Trooper (also have a Command Centurion ensemble from BSG TOS - but that's a different Empire!)
Yes the M-105ПA was better for dogfights at the lower attitudes. The M-105 engine series was "equipped" with the device called by Russian " ПЦН - Приводной Центобежный Нагнетатель" what can be simply cansidered to be a centrifugal compressor or supercharger. It was two-speed device. The first speed was started at 2000m while the second one at 4000m. By reduction of these calculated altitudes it was possible to increase the pressure at the lower levels. This resulted in increasing of the power at the lower altitudes.
And here is another chart form the mentioned book. It may come in handy as well...
View attachment 626871
the source: Авиационный двигатель М-105.
Which the data tables do you use for the ДБ-240?