<?xml version="1.0"?>
<!--
  File:     Argus_As_10.xml
  Author:   Ron Jensen

Specifications (Argus As 10 C)
General characteristics

    * Type: 8-cylinder, air-cooled, 90 degree inverted Vee piston aircraft engine
    * Bore: 120 mm (4.72 in)
    * Stroke: 140 mm (5.5 in)
    * Displacement: 12.667 l (773 in3)
    * Length: 1,105 mm (43.51 in)
    * Height: 936 mm (36.85 in)
    * Dry weight: 213 kg (470 lb)

Components

    * Valvetrain: Two valves per cylinder.
    * Fuel system: Two Sun carburetors adapted for aerobatics
    * Fuel type: 80 octane
    * Cooling system: Air

Performance

    * Power output:
          o 179 kW (240 hp) at 2,000 rpm
    * Specific power: 14.8 kW/L (0.31 hp/in3)
    * Compression ratio: 5.9:1
    * Specific fuel consumption: 235 gr/(hp*h); 0.518 lb/(hp*h)
    * Power-to-weight ratio: 0.835 kW/kg (0.51 hp/lb)

-->

<piston_engine name="Argus_As_10">
  <minmp unit="INHG">          6.0 </minmp>
  <maxmp unit="INHG">         30.0 </maxmp>
  <displacement unit="IN3"> 773.00 </displacement>
  <maxhp unit="WATTS">      179000 </maxhp>
  <cycles>         4.0 </cycles>
  <idlerpm>      500.0 </idlerpm>
  <maxrpm>      2000.0 </maxrpm>
  <maxthrottle>    1.0 </maxthrottle>
  <minthrottle>    0.05 </minthrottle>
  <bsfc unit="LBS/HP*HR"> 0.518</bsfc>
  <volumetric-efficiency> 0.7625 </volumetric-efficiency>
</piston_engine>
