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classification system then in use in
Imperial Germany. It also employed reduction gearing. When the reliability of the engine proved disappointing, it was supplanted in production by the unrelated six-cylinder
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117:. Specifically, the long crankshaft used in extending the original straight-six design to a straight-eight proved susceptible to breakage.
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6-cylinder design and developed 162 kW (217 hp), making it a Class IV motor under the
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90:(DMG) and used on a small number of German aircraft during
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The design was based around the pistons of the ubiquitous
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8-cylinder water-cooled inline aircraft piston engine
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323:German & Austro-Hungarian Aero Engines of WWI
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306:Kroschel, Gunter and Helmust Stützer. (1977)
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325:. Vol. 2. n. p.: Aeronaught Books.
308:Die deutschen Militarflugzeuge 1910-1918
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310:Wilhelmshaven: Lohse-Eissing Mittler.
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448:1910s aircraft piston engines
279:162 kW (217 hp) at 1,400 rpm
87:Daimler Motoren Gesellschaft
51:Daimler Motoren Gesellschaft
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443:Mercedes aircraft engines
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321:Düsing, Michael (2022).
295:List of aircraft engines
191:General characteristics
80:, liquid-cooled inline
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98:Design and development
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16:Aircraft engine model
40:Inline piston engine
226:19.7 L (1,202.4 in)
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332:978-1-953201-52-2
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386:aircraft engines
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244:1,040 mm (41 in)
232:1,990 mm (78 in)
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315:Further reading
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264:Cooling system:
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253:365 kg (800 lb)
217:160 mm (6.3 in)
208:140 mm (5.5 in)
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115:Mercedes D.IVa
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160:Albatros C.V
121:Applications
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271:Performance
92:World War I
437:Categories
301:References
258:Components
249:Dry weight
170:Gotha G.II
155:AGO C.VIII
186:Data from
140:AEG G.III
84:built by
383:Mercedes
284:See also
175:LVG C.IV
150:AGO C.II
242:Height:
230:Length:
165:DFW R.I
145:AEG R.I
135:AEG C.V
109:IdFlieg
76:was an
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236:Width:
213:Stroke
54:(DMG)
422:D.IVa
412:D.III
197:Type:
104:D.III
36:Type
22:D.IV
417:D.IV
407:D.II
327:ISBN
204:Bore
72:The
402:D.I
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Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
