Hi DT,
The engines of the Hs-129 cannot match these parameters from the engine handbook:
In Il-2 the max RPMs possible are about 2700. Setting pressure to 1.1 ATA give RPMs of only 2000 max.
According to Azimech:
Quote:
Startleistung = Take Off
Steig- und Kampfflugleistung = Climb and Combat Power
Höchstzulässige Dauerleistung = Max Continious Power
Höchstsparleistung = Economy Cruise
dauernd = continious
Ladedruck = manifold pressure
Drehzahl = RPM
PS= horsepower
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Full manual is here:
http://www.cockpitinstrumente.de/index-englisch.htm
Type Gnome-Rhone in the search box on the right, and the document PDF should be the first result.