• Source: Argus As 10

The Argus As 10 was a German-designed and built, air-cooled 90° cylinder bank-angle inverted V8 "low power" aircraft engine, used mainly in training aircraft such as the Arado Ar 66 and Focke-Wulf Fw 56 Stösser and other small short-range reconnaissance and communications aircraft like the Fieseler Fi 156 Storch during, and shortly after World War II. It was first built in 1928.




Variants


As 10C

As 10C-1

As 10E
Optional-output version of the As 10C, delivered with either a 240 PS (177 kW) or 270 PS (199 kW) rating (achieved by increasing maximum rpm).
As 10E-2
The proposed powerplant of the Pilatus P-1 trainer project.
As 401
Supercharged As 10 with rated output at 3,000 m (9,843 ft), also fitted with hydraulically actuated variable pitch propeller.
Salmson 8As-00
Postwar production of the Argus As 10 in France
Salmson 8As-04
Postwar production of the Argus As 10 in France




Applications



AGO Ao 192
Arado Ar 66
Arado Ar 76
Dornier Do 12
Farman F.510 Monitor II
Fieseler Fi 156 Storch
Focke-Wulf Fw 56 Stösser
Focke-Wulf Fw 58
Gotha Go 145
Henschel Hs 121
Kayaba Ka-1 Imperial Japanese Army Observation autogiro
Klemm Kl 151
Messerschmitt Bf 108 Taifun
Rogozarski SIM-XIV-H
Siebel Si 201




Specifications (Argus As 10 C)



Data from Jane's All the World's Aircraft 1938, Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944




= General characteristics

=
Type: inverted V-8 air-cooled inverted 90° piston engine
Bore: 120 mm (4.724 in)
Stroke: 140 mm (5.512 in)
Displacement: 12.667 L (772.99 cu in)
Length: 1,105 mm (43.50 in)
Width: 880 mm (34.65 in)
Height: 718 mm (28.27 in)
Dry weight: 213 kg (470 lb) dry
232 kg (511 lb) wet, equipped




= Components

=
Valvetrain: Two under-head valves per cylinder, operated by pushrods and rockers.
Fuel system: Two Sun carburetors adapted for aerobatics
Fuel type: 80 octane
Oil system: Dry sump, one pressure pump at 1.25–6 atm (1.27–6.08 bar; 18.4–88.2 psi) and two scavenge pumps
Cooling system: Air




= Performance

=
Power output:
240 PS (237 hp; 177 kW) at 2,000 rpm (5 minutes) at sea level
220 PS (217 hp; 162 kW) at 1,940 rpm (30 minutes) at sea level
200 PS (197 hp; 147 kW) at 1,890 rpm (max continuous) at sea level
Specific power: 18.95 PS/L (0.3063 hp/cu in; 13.94 kW/L)
Compression ratio: 5.9:1
Specific fuel consumption: 0.23 kg/PSh (0.51 lb/(hp⋅h); 0.31 kg/kWh) at max continuous
Oil consumption: 0.008 kg/PSh (0.018 lb/(hp⋅h); 0.011 kg/kWh) at max continuous
Power-to-weight ratio: 1.124 PS/kg (0.503 hp/lb; 0.827 kW/kg)0.835 kW/kg (0.51 hp/lb)
B.M.E.P.: 7.5 atm (760 kPa; 110 psi)




See also



Related lists

List of aircraft engines




References






= Notes

=




= Bibliography

=

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