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Argus As II

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This is an old revision of this page, as edited by Cydebot (talk | contribs) at 00:47, 8 May 2019 (Robot - Moving category Aircraft piston engines 1910–1919 to Category:1910s aircraft piston engines per CFD at Wikipedia:Categories for discussion/Log/2019 April 19.). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

As II
Argus As.II artist drawing
Type Piston aircraft engine
Manufacturer Argus Motoren
First run 1914

The Argus As II was a six-cylinder, in-line, water-cooled, aircraft engine produced in Germany by Argus Motoren in 1914.[1]

Applications

Specifications

General characteristics

  • Type: Six-cylinder, upright, inline, liquid-cooled piston engine
  • Bore: 130 mm
  • Stroke: 130 mm

Components

  • Valvetrain: Overhead-valve, two valves per cylinder, pushrod operated
  • Fuel system: Twin carburettors
  • Oil system: Pressure feed

Performance

  • Power output: 120 hp (89 kW) at 1,350 rpm[1][3]

See also

Related lists

References

  1. ^ a b c d "Argus As.II 120cv engine". Trimble 3D Warehouse. Retrieved 9 July 2013.
  2. ^ Early Aviator: Aeroplanes 1914-1918
  3. ^ Ruudleeuv: Dubendor Air Force Center Museum
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