Aircraft engine: Argus As-8 (cross section)
Germany
inline engine
1929/1930
Configuration | 4-cylinder inverted inline |
Cooling | air-cooled |
Displacement | 6.3 l (366 cu. in) |
Compression ratio | 5.3 |
Weight | 113 kg (249 lb) |
Maximum power | 95 hp at 1,600 rpm |
Climb power | 80 hp at 1,400 rpm |
The engine was designed at the Argus Motoren Gesellschaft under the supervision of Dr M. Christian. It was used in the Albatros L.101 aircraft, which took part in the Challenge contest in 1930.
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