Hi all,
re : the G-14 charts, I'd have to find them first, I don't have them scanned yet. But based on the 109K charts, and the effect of weight difference (apprx. -100kg = + 1 m/sec), it's fairly accurate.
George,
I think the chart you refer to is the one that floats around the net, I think it's the the one that shows the DC engine 'o. MW' (=ohne MW, without MW50 injection), just relying on C-3 fuel alone. Without MW50 injection, the DC would develop at SL :
When set to 1.98ata, running at 1.8ata : 1725 PS
When set to 1.8ata, running at 1.8ata : 1800 PS
This explains why the '1.98ata' climb rates are lower - it merely refers to an engine setup when 1.98ata maximum boost was set (which would require C3 + MW), but only C3 was used.. I guess it's not the proper setup, ie. spark plug timing must have been different as well for 1.98ata. I can't confirm that yet, but seems very likely.
Note that the DC could run at various settings, the above two w/o MW50 injection (esp. 1.98/1.8) are atypical and rather theoretical - the only case I can think of this happening when the rear MW tank was used for extra fuel storage instead for 118 liter extra tankage.
The chart I (also) have shows the
Sondernotleistung with MW injection at 1.98ata. SL RoC is 24.5m/sec, increasing to 25 at around 600m altitude.
Please contact me both of you at
kurfurst@atw.hu. I cannot promise I will reply immidiately, but I will when I have time. Especially George, I have some Russian 109 stuff which I can't translate exactly.
