Aero Engine Data Sheets

German Aero Engines: Page 126 of 140

N/A = Not Applicable --- NA = Info Not available

Maker	Junkers 205C	Junkers 205D	----	----	----	----	----
Arrangement	Inline	Inline	----	----	----	----	----
Cooling	Liquid	Liquid	----	----	----	----	----
No of Cyls	6	6	----	----	----	----	----
Bore/Stroke	4.13" x 6.30"	4.13" x 6.30"	----	----	----	----	----
Displacement	1013.8 cu ins	1013.8 cu ins	----	----	----	----	----
Comp Ratio	17:1	17:1	----	----	----	----	----
bmep Cruise	100	105	----	----	----	----	----
Blower ratio	N/A	N/A	----	----	----	----	----
Cyl Material	Steel	Steel	----	----	----	----	----
Valves per cyl	Ports	Ports	----	----	----	----	----
Valve Arr.	Ports	Ports	----	----	----	----	----
HP max - not Take-Off	NA	NA	----	----	----	----	----
@ RPM	NA	NA	----	----	----	----	----
@ Altitude	NA	NA	----	----	----	----	----
HP Take-Off	600	700	----	----	----	----	----
@ RPM	2200	2600	----	----	----	----	----
HP Cruise	510	590	----	----	----	----	----
@ RPM	2000	2200	----	----	----	----	----
Fuel Octane	Diesel	Diesel	----	----	----	----	----
Prop Drive	Geared	Geared	----	----	----	----	----
Dry Weight	1146.6 lbs	1146.6 lbs	----	----	----	----	----
lb/Cruise HP	2.24	1.94	----	----	----	----	----
Carb(s)	Injection	Injection	----	----	----	----	----
Ignition	Diesel	Diesel	----	----	----	----	----
Starting Method	Own, Comp Air	Own, Comp Air	----	----	----	----	----
Length	76.50"	76.50"	----	----	----	----	----
Height/O.D.	52.17"	52.17"	----	----	----	----	----
Width	21.54"	21.54"	----	----	----	----	----
Bed centres	NA	NA	----	----	----	----	----
Mount Dia	NA	NA	NA	NA	NA	NA	NA
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Let me know if any of the above does not read true, or if you have information that does not agree. Wherever possible, I will update these pages on a regular basis as data comes in.