Armstrong Whitworth Siskin

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Armstrong Whitworth Siskin
The Royal Air Force in the Middle East, 1919-1939 HU70791.jpg
Siskin Mk.III
Type: Fighter plane
Design country:

United KingdomUnited Kingdom United Kingdom

Manufacturer:

Armstrong Whitworth Aircraft

First flight:

1919

Commissioning:

1923

Number of pieces:

485

The Armstrong Whitworth Siskin was a British biplane - fighter of the interwar period .

history

The development work on a successor model for the slowly obsolete fighter aircraft of the Royal Flying Corpsstarted in 1918. Siddeley and Armstrong Whitworth each presented a prototype. They didn't differ that much in appearance, but just in one decisive point. Siddeley relied on a weaker engine, the Royal Aircraft RAF.8 with 300 hp, which the company even had to buy in, while Armstrong Whitworth designed and produced its own much more powerful engine. Its name was Jaguar IV and the output was significantly higher at 420 hp. A total of 360 machines were produced by Armstrong and under license from Bristol, Vickers, Gloster and Blackburn. From 1923 the aircraft were introduced by the British Air Force as the Siskin III. From 1927 to 1930 the Siskin was the backbone of British home defense. From then on, better models like the Bristol Bulldog or the Gloster Gauntlet were available.

The plane

According to the requirements of the UK Aviation Department , the Siskin was an all-metal construction. The cockpit was still open. The armament was housed in the fuselage and shot through the propeller circle. Here, too, no tail wheel has been used at the rear, just a grinding spur. The radial engine was not disguised. This meant that even lighter hits could have caused damage to the aircraft. Armoring of the engine block as a retrofit kit was never developed. However, the Siskin never had a combat mission, which is why this circumstance was not particularly important.

production

The Armstrong Whitworth Siskin was built in series by five companies (Armstrong Whitworth, Whitley Abbey; Bristol, Filton; Blackburn, Bough; Gloster; Vickers, Weybridge).

Approval of the Armstrong Whitworth Siskin by the RAF:

Manufacturer version 1923 1924 1925 1926 1927 1928 1929 1930 total
AW Mk.III 4th 41 4th 8th         57
AW Mk.IIIDC     6th     11 36   53
AW Mk.IIIA     1 13 53 21st     88
Bristol Mk.IIIA           46 22nd 15th 83
Blackburn Mk.IIIA           42     42
Gloster Mk.IIIA         3 39 22nd 10 74
Vickers Mk.IIIA             27 25th 52
total   4th 41 11 21st 56 159 107 50 449

Military use

Canada 1921Canada Canada
EstoniaEstonia Estonia
SwedenSweden Sweden
United KingdomUnited Kingdom United Kingdom

Technical specifications

Parameter Data
crew 1
span 10.11 m
length 7.72 m
Engine Armstrong Whitworth Jaguar IV radial engine
power 420 hp / 313 kW
Top speed 251 km / h
Flight duration approx. 3 h
Summit height 8,230 m
Armament two built-in, forward-firing 7.7 mm Vickers machine guns ,
underwing mounts for 4 × 9 kg bombs

literature

  • Michael Sharpe: Biplane, Triplane & Seaplanes. Gondromverlag, Bindlach 2001, ISBN 3-8112-1872-7 .
  • Oliver Tapper: Armstrong Whitworth Aircraft since 1913. Putnam, London 1988, ISBN 0-85177-826-7 .

Web links

Commons : Armstrong Whitworth Siskin  - Collection of Images, Videos and Audio Files

Individual evidence

  1. ^ Thompson, Dennis: Royal Air Force Aircraft J1 – J9999 , Tonbridge 1987