Argus As 8

1930s German piston aircraft engine


title: "Argus As 8" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["air-cooled-aircraft-piston-engines", "argus-aircraft-engines", "1930s-aircraft-piston-engines", "inverted-aircraft-piston-engines"] description: "1930s German piston aircraft engine" topic_path: "general/air-cooled-aircraft-piston-engines" source: "https://en.wikipedia.org/wiki/Argus_As_8" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary 1930s German piston aircraft engine ::

::data[format=table title="infobox aero engine"]

FieldValue
nameAs 8
imageArgus As 8 1.jpg
captionArgus As 8 aircraft engine
engine_typePiston aircraft engine
manufacturerArgus Motoren
::

|name=As 8 |image=Argus As 8 1.jpg |caption=Argus As 8 aircraft engine |engine_type=Piston aircraft engine |manufacturer=Argus Motoren |first_run= |major_applications= |number_built = |developed_from = |developed_into = |variants_with_their_own_articles =

The Argus As 8 was a four-cylinder, air-cooled, inverted inline aircraft engine produced in Germany by Argus Motoren in the 1930s.

Variants

;As 8A:Initial production version 95 hp maximum for 5 minutes, 80 hp continuous. ;As 8B:A more powerful variant developing 135 hp maximum for 5 minutes, 115 hp continuous. ;As 8R:A variant produced for sport aircraft, particularly for competition use, developing 150 hp for take-off. Featuring: :*Increased compression ratio, from 5.36 to 5.8 :*Improved cooling by increasing the numbers of cooling fins at the cylinder head and the cylinder body :*Increasing the heat dispersing area of the pistons :*Improved crankcase and oil cooling :*Improved cylinder charging :*Modified valve timing

Applications

Specifications (As 8B)

and start a new, fully-formatted line with -- |ref=Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944, Argus AS-8R |type=4-cylinder inverted air-cooled in-line piston engine |bore=120 mm |stroke= 140 mm |displacement=6.332 L |length=1075 mm without airscrew hub |diameter= |width=470 mm |height=731 mm |weight=116 kg dry ::::128.4 kg equipped |valvetrain=Overhead valves operated by pushrods and rockers |supercharger= |turbocharger= |fuelsystem=One down-draught carburretor |fueltype=80 Octane Aviation gasoline |oilsystem=Pressure feed at 3 - |coolingsystem=Air-cooled |power=

:*135 PS at 2,200 rpm (5 minutes) at sea level :*125 PS at 2,150 rpm (30 minutes) at sea level :*115 PS at 2,090 rpm (max continuous) at sea level |specpower=21.3 PS/L |compression=5.35:1 |fuelcon= |specfuelcon=

:*0.235 kg/PSh at maximum rpm :*0.230 kg/PSh at maximum continuous rpm |oilcon=0.008 kg/PSh at maximum continuous rpm |power/weight=1.149 PS/kg

  • B.M.E.P.: 7.7 atm |designer= |reduction_gear=

|general_other= |components_other= |performance_other=

References

References

  1. Schneider, Helmut (Dipl.Ing.). (1944). "Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944". Herm. Beyer Verlag.
  2. "Argus AS-8 R:".

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air-cooled-aircraft-piston-enginesargus-aircraft-engines1930s-aircraft-piston-enginesinverted-aircraft-piston-engines