Argus As 411

Last updated
As 411
Argus As 411 A 1.jpg
Preserved Argus As 411
Type Piston aircraft engine
Manufacturer Argus Motoren
Major applications Arado Ar 96
Focke-Wulf Fw 189
Number built2,600

The Argus 411 was an air-cooled, inverted-V12 aircraft engine developed by Argus Motoren in Germany during World War II. [1]

Contents

Design and development

The As 411 was a refined and more powerful version of the Argus As 410. Most 411 production was undertaken by Renault in occupied Paris, these engines were used to power the Siebel Si 204 and the postwar Dassault MD 315 Flamant. It developed 600 PS (592 hp, 441 kW) at 3,300 rpm

Following the end of World War II, Renault continued to manufacture the engine as the Renault 12S. After the merger of the French aircraft engine manufacturers into SNECMA in 1945, production continued under the new designation SNECMA 12S.

Variants

Argus As 411A in Deutsches Museum Munchen Argus As 411A.jpg
Argus As 411A in Deutsches Museum München
As 411
A refined and more powerful version of the Argus As 410.
Renault 12S
Production of the As 411 after World War II in France.
SNECMA 12S
(a.k.a. SNECMA Renault 12S) Designation change on the formation of SNECMA.
SNECMA 12T
(a.k.a. SNECMA Renault 12T) Refined version of the 12S with new pistons, cylinders and revised induction system.
SNECMA 12T-303
Dassault propeller
SNECMA 12T-312
Ratier propeller

Applications

Specifications (SNECMA 12S)

Data fromAircraft engines of the World 1953 [2]

General characteristics

Components

Performance

Take-off:450 kW (600 hp) at 3,300 rpm / 1,325 mmHg (52.2 inHg) +5.0 kg (11.1 lb) boost
Normal:330 kW (440 hp) at 3,250 rpm at 2,400 m (7,900 ft)
Cruising, max:260 kW (350 hp) at 3,100 rpm at 2,600 m (8,500 ft)

See also

Comparable engines

Related lists

Related Research Articles

<span class="mw-page-title-main">Junkers Jumo 210</span> V-12 piston aircraft engine family by Junkers

The Jumo 210 was Junkers Motoren's first production inverted V12 gasoline aircraft engine, first produced in the early 1930s. Depending on the version it produced between 610 and 730 PS and can be considered a counterpart of the Rolls-Royce Kestrel in many ways. Although originally intended to be used in almost all pre-war designs, rapid progress in aircraft design quickly relegated it to the small end of the power scale by the late 1930s. Almost all aircraft designs switched to the much larger Daimler-Benz DB 600, so the 210 was produced only for a short time before Junkers responded with a larger engine of their own, the Junkers Jumo 211.

<span class="mw-page-title-main">Dassault MD 315 Flamant</span> Type of aircraft

The Dassault MD 315 Flamant is a French light twin-engined transport airplane built shortly after World War II by Dassault Aviation for the French Air Force.

<span class="mw-page-title-main">Chrysler IV-2220</span> World War II–Era experimental aircraft engine

The Chrysler XIV-2220 was an experimental 2,500 hp, 2,220 cubic inch liquid-cooled inverted-V-16 World War II aircraft engine. Although several aircraft designs had considered using it, by the time it was ready for use in 1945 the war was already over. Only a few engines were built by Chrysler during a program that started in 1940, and it retained its 'X' designation the entire time as the XIV-2220, later XI-2220. The IV-2220 is historically important as it was Chrysler's first hemi, a design that would re-appear in 1950s Chrysler performance automobiles, make drag racing headlines in the 1960s, and continue into the 2000s.

<span class="mw-page-title-main">Allison V-3420</span> Large experimental piston aircraft engine

The Allison V-3420 was a large experimental piston aircraft engine, designed in 1937 by the American Allison Engine Company.

<span class="mw-page-title-main">Gnome-Rhône Mistral Major</span> 1930s French radial aircraft engine

The Gnome-Rhône 14K Mistral Major was a 14-cylinder, two-row, air-cooled radial engine. It was Gnome-Rhône's major aircraft engine prior to World War II, and matured into a highly sought-after design that would see licensed production throughout Europe and Japan. Thousands of Mistral Major engines were produced, used on a wide variety of aircraft.

<span class="mw-page-title-main">Fiat A.80</span> 1940s Italian piston aircraft engine

The Fiat A.80 was an 18-cylinder, twin-row, air-cooled, radial aircraft engine produced during World War II. Rated at 750 kW (1,000 hp), it was a more powerful development of the 14-cylinder Fiat A.74.

<span class="mw-page-title-main">Hirth HM 508</span> 1930s German 8-cylinder inverted-V aircraft engine

The Hirth HM 508 was an air-cooled, eight-cylinder, 60° cylinder bank angle inverted-V aircraft engine built in Germany in the 1930s. It had a bore and stroke of 105 mm × 115 mm and developed 210 kW (280 hp) at 3,000 rpm.

<span class="mw-page-title-main">Argus As 410</span> 1930s German piston aircraft engine

The Argus As 410 was a German air-cooled inverted V-12 aircraft engine that was first produced by Argus Motoren in 1938.

<span class="mw-page-title-main">Armstrong Siddeley Tiger</span> 1930s British piston aircraft engine

The Armstrong Siddeley Tiger was a British 14-cylinder air-cooled aircraft radial engine developed by Armstrong Siddeley in the 1930s from their Jaguar engine. The engine was built in a number of different versions but performance and dimensions stayed relatively unchanged. The Tiger VIII was the first British aircraft engine to use a two-speed supercharger.

<span class="mw-page-title-main">Armstrong Siddeley Cougar</span>

The Armstrong Siddeley Cougar was an aero engine developed by Armstrong Siddeley in 1945. The design was a departure from earlier Armstrong Siddeley engines in many ways, it was the company's only nine-cylinder radial design. Although the engine was tested it did not find an aircraft application and was not produced.

The Hirth HM 512 was a 12-cylinder development of the earlier, 6-cylinder HM 506, produced in the late 1930s. Both were supercharged, inverted V, air-cooled engines.

<span class="mw-page-title-main">Isotta Fraschini Asso XI</span>

The Asso XI was a family of water-cooled, supercharged V12 piston aeroengines produced in the 1930s by Italian manufacturer Isotta Fraschini, and fitted on a number of aircraft types built by CANT, Caproni and others.

The Renault 4P, also called the Renault Bengali Junior, was a series of air-cooled 4-cylinder inverted inline aero engines designed and built in France from 1927, which produced from 95 hp (71 kW) to 150 hp (110 kW).

<span class="mw-page-title-main">SNECMA 14R</span> Radial piston aircraft engine

The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the Gnome-Rhône 14N. The 14N radial engine was itself an improved version of the popular pre-war Gnome-Rhône 14K Mistral Major series; designed and manufactured by Gnome et Rhône, a major French aircraft engine manufacturer whose origins pre-date the First World War.

<span class="mw-page-title-main">Walter Sagitta</span> 1930s Czech piston aircraft engine

The Walter Sagitta was a Czechoslovakian, air-cooled, inverted V-12 engine that first ran in 1937. This was one of several smaller, low-mass medium power pre-war V-12 engines produced. With a displacement of 18.4 liters, it produced up to 373 kW at 2,500 rpm.

The Béarn 6 was a six-cylinder air-cooled piston aircraft engine produced in France in the late 1930s, 1940s and early 1950s.

The Renault 6P, also called the Renault Bengali, was a series of air-cooled 6-cylinder inverted in-line aero engines designed and built in France from the late 1920s, which produced from 130 kW (180 hp) to 200 kW (270 hp).

<span class="mw-page-title-main">Renault 6Q</span> 1930s French piston aircraft engine

The Renault 6Q, also called the Renault Bengali 6, is an air-cooled inverted in-line six-cylinder, aircraft piston engine, producing about 160 kW (220 hp) continuous power. It was designed and built in France and produced for more than ten years after its homologation in 1936, with large numbers built during World War II.

<span class="mw-page-title-main">Isotta Fraschini Beta</span> 1940s Italian aircraft piston engine

The Isotta Fraschini Beta was an air cooled aircraft engine produced by the Italian engineering company Isotta Fraschini in the 1940s. Isotta Fraschini derived the Beta inverted 6-cylinder in-line aircraft engine from the V-12 Gamma. The engine saw limited production for aircraft, including the Nardi FN.316 and Ambrosini SAI.7, but was generally unsatisfactory in service.

<span class="mw-page-title-main">Renault 12R</span> 1930s French piston aircraft engine

The Renault 12R was an air-cooled inverted V12 aircraft engine developed by the French engineering company Renault in the 1930s. The design was based on mounting two 6Q six-cylinder engines on a single crankshaft. In production, the engine was rated between 450 and 500 hp, although a high performance version built for the sole Caudron C.712 racing special produced 730 hp (540 kW). More than one third of production went to power the Caudron C.714 light fighter that fought in the early stages of World War II for the French and Polish Air Forces.

References

  1. Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2nd ed.). Cambridge, England: Patrick Stephens Limited. p. 16. ISBN   978-1-85260-163-8.
  2. Wilkinson, Paul H. (1953). Aircraft engines of the World 1953 (11th ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 296–297.

Further reading