Argus As II

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. 1 2 3 4 "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
  • "Der Argus Flugmotor. Argus As II, As III and As IV aero engine manual". 1916. Retrieved 29 March 2013.
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