Blackburn Shark

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Shark
RCAF Blackburn Shark Mk II
Role torpedo-spotter-reconnaissance aircraft
National origin United Kingdom
Manufacturer Blackburn Aircraft
First flight 24 August 1933
Introduction 1934
Retired 1945
Primary users Royal Navy
Royal Air Force
Royal Canadian Air Force
Portuguese Navy
Produced 1937–1939
Number built 269

The Blackburn Shark was a carrier-borne torpedo bomber designed and built by the British aviation manufacturer Blackburn Aircraft. It was originally known as the Blackburn T.S.R., standing for "torpedo-spotter-reconnaissance", in reference to its intended roles. The Shark was the last of Blackburn's biplane torpedo bombers.[1]

The prototype Shark performed its

Dunkirk Evacuation and the Japanese invasion of British Malaya
. During 1945, the final Sharks were withdrawn from service.

Design and development

Background

The Blackburn T.9 Shark has its origins within the early 1930s as a private venture by the company.

Second World War.[2]

The T.S.R. represented a substantial departure from Blackburn's previous naval aircraft designs, as the design team had opted to eliminate almost all use of streamlined bracing wires in favour of slanted struts.

pneumatic wheel brakes.[2] The design process had been aided by operational experienced gained from the Blackburn Baffin. Features, such as the camber-changing flaps and fuselage construction, were derived from earlier prototypes.[3]

Initially, the design of the T.S.R featured open cockpits, which were heated by an exhaust pipe muff.

Lewis Gun mounted on a Scarff ring in the rear cockpit, with provision for a 1,500 lb (680 kg) torpedo or equivalent bombload carried externally.[3][4]

The fuselage was strengthened to withstand catapult launches and divided into watertight compartments. Structural elements included stainless steel tubular spars and light alloy ribs; similar materials were used for the entire tail section save for the Alclad-plated fin.[5] The majority of the flying surfaces had fabric coverings; the wing tips were detachable as to allow their easy replacement if damaged. The main fuel tanks were not integral to the structure; instead, two detachable tanks composed of duralumin were carried in separate watertight compartments forward of the pilot, housing up to 182.5 gallons of fuel.[6] The aircraft had a range of 623 miles normally, but this could be extended to 1,130 miles via the use of a cylindrical tank, attached to the torpedo crutches, that was capable of holding up to 150 gallons of additional fuel.[3]

Into flight

On 24 August 1933, Blackburn's B-6 prototype, powered by with a 700 hp (520 kW) Armstrong Siddeley Tiger IV engine, made its maiden flight at Brough.[4] Following the completion of manufacturer trials, during which the engine was enclosed in a long-chord cowling, this prototype was delivered to the Aeroplane and Armament Experimental Establishment (A&AEE) at RAF Martlesham Heath for an official performance evaluation on 26 November 1933.[6] During the following year, after the conclusion of testing at Martlesham, it was transferred to Gosport ahead of deck landing trials on board the aircraft carrier HMS Courageous. These having been deemed successful as well, the prototype was taken up by the Directorate of Technical Development.[6]

During August 1934, Blackburn received an initial production order for 16 aircraft to be produced for the FAA.[6] One month later, limited production had already commenced. During October 1934, the name Shark I was officially sanctioned; around this time, a series of modifications were implemented, the most visible of which was a lengthened engine cowling that enclosed the exhaust collector ring.[6] Amongst the modifications needed was for the aircraft to be convertible to a seaplane configuration, thus the prototype was overhauled and outfitted with twin floats equipped with shock absorbers. In this configuration, early test flights were conducted at Brough during April 1935; a successful series of sea trials took place at the Marine Aircraft Experimental Establishment Felixstowe.[1]

Blackburn was issued contract No. 334315/34 in conjunction with the new Specification 13/35. I, along with the additional contract No. 510994/35 to Specification 19/36, which was issued in January 1937. Even more contracts soon followed, leading to the rate of production exceeding that of numerous preceding Blackburn aircraft. During a three-year production run, a total of 238 Sharks were delivered to the FAA, comprising 16 Mk I (Tiger IV), 126 Mk II (760 hp (570 kW) Tiger VI) and 95 Mk III (760 hp (570 kW) Tiger VI).

Rotol wooden propellers. Late on in production, assembly from components produced elsewhere took place at Blackburn's new factory in Dumbarton, Scotland, after which the completed airframes were transported by road to the Clyde for flight testing.[8]

Operational history

Fleet Air Arm

Fleet Air Arm Blackburn Shark in company with a Westland Wapiti, seen flying over HMS Courageous

During May 1935, the Shark entered service with 820 Naval Air Squadron, replacing its Fairey Seals, aboard HMS Courageous.[9] During the following year, it also equipping an additional two squadrons, 810 and 821.[7] The FAA opted to actively deploy the Shark both in its landplane configuration on board the Royal Navy's aircraft carriers and as a seaplane on its battlecruisers, such as HMS Warspite and HMS Repulse; in the latter capacity, it would either be catapult-launched or lowered over the side to take off from the water, dependent on available equipment. Its seaworthiness was a particular point of praise, possessing favourable rough water handling and buoyancy characteristics.[10]

Frontline operations involving the Shark were curtailed after only a relatively short timespan, as the type had started to be replaced by the more capable

Lee-on-Solent. 20 Sharks were converted by Blackburn into target tugs and saw use at units in Abbotsinch, Gosport, Crail, and Arbroath to help train pilots, starting in 1939.[12] On 4 January 1939, two Sharks were taken up by No. 4 Anti-Aircraft Co-Operation Unit in Seletar, Singapore.[13]

During the

flares, they were otherwise unarmed; these operations were hindered and eventually stopped by poor weather conditions.[14] Widespread use of the Shark III for the training of aerial observers and navigators proceeded as far afield as Trinidad; its use in this role continued to as late as 1942.[15]

Numerous Sharks would eventually be based at

RAF Seletar as target tugs. During January 1942, the type was used to conduct patrol missions and even bombing raids against units of the Imperial Japanese Army as it advanced into Malaya.[16][15]

Overseas operators

A pair of Canadian Sharks, circa 1940

On 10 April 1935, Blackburn successfully secured a contract over rival firms from the

River Tagus outside Lisbon for coastal defense duties.[17] On 22 October 193, a long distance non-stop flight was conducted by a Portuguese Shark between Bom Succeso and RAF Calshot, carrying a diplomatic dispatch to London and returning six days later.[18]

During 1936, the Royal Canadian Air Force (RCAF) purchased seven Blackburn Shark II (760 hp/570 kW Tiger VI), the first four of which were shipped in September of that year.[18] It was initially flown by No 6 (TB) Squadron, later operating as No 6 (BR) Sqn, to perform shipping patrols off the west coast of Canada. The type was reportedly appreciated for its rugged design and ease of maintenance, particular when operated from remote areas far from well-equipped workshops.[18] The Shark became an element of a wider plan to bolster Canada's domestic production of aircraft; during early 1939, a pair of Shark IIIs (800 hp/600 kW Pegasus III) were supplied by Blackburn to serve as pattern aircraft for a further 17 aircraft that were locally produced by Boeing Aircraft of Canada at their Vancouver facility except for the stainless steel spars provided by Boulton Paul from the UK.[19]

The Canadian-built aircraft were powered by 840 hp (630 kW) Pegasus IX engines and were supplied to Nos 6 and 4 (BR) Squadrons. However, by the time quantity manufacturing had been attained in Vancouver, it was becoming increasingly recognised that the Shark was too obsolete to fulfil Canada's ongoing wartime needs.[20] Nevertheless, these aircraft produced were deployed for naval reconnaissance and the escorting of friendly shipping near to Canada. The last of the RCAF's Sharks, some of which were operated as floatplanes, were withdrawn from service in August 1944, after which five aircraft were transferred to the RN Air Observers' School in Trinidad.[21]

Variants

  • B-3 : Torpedo-bomber prototype.
  • B-6 : Shark prototype.
  • Shark Mk I : Two- or three-seat torpedo bomber, reconnaissance aircraft for the
    Armstrong Siddeley Tiger IV
    radial piston engine.
  • Shark Mk II : Two- or three-seat torpedo bomber, reconnaissance aircraft for the Royal Navy and
    Armstrong Siddeley Tiger VI
    radial piston engine.
  • Shark Mk IIA : Two- or three-seat torpedo bomber, reconnaissance floatplanes for the
    Armstrong Siddeley Tiger VIC
    radial piston engine. Six built.
  • Shark Mk III : Two- or three-seat torpedo bomber, reconnaissance aircraft for the Royal Navy. Fitted with a glazed canopy and dual controls for crew training. Powered by an 800 hp (600 kW)
    Bristol Pegasus III
    radial piston engine.

Operators

 Canada
 Portugal
 United Kingdom

Specifications (Shark Mk II)

Data from The British Bomber since 1914[24]

General characteristics

  • Crew: 3
  • Length: 35 ft 3 in (10.74 m)
  • Wingspan: 46 ft (14 m)
  • Height: 12 ft 1 in (3.68 m)
  • Wing area: 489 sq ft (45.4 m2)
  • Empty weight: 4,039 lb (1,832 kg)
  • Gross weight: 8,111 lb (3,679 kg)
  • Powerplant: 1 ×
    Armstrong Siddeley Tiger VI
    14-cylinder air-cooled radial piston engine, 760 hp (570 kW)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 150 mph (240 km/h, 130 kn)
  • Cruise speed: 118 mph (190 km/h, 103 kn)
  • Range: 625 mi (1,006 km, 543 nmi)
  • Endurance: four hours and 54 minutes
  • Service ceiling: 15,600 ft (4,800 m)
  • Rate of climb: 895 ft/min (4.55 m/s)
  • Time to altitude: 6,500 ft (2,000 m) in 7 minutes 6 seconds
  • Wing loading: 16.6 lb/sq ft (81 kg/m2)
  • Power/mass: 0.0937 hp/lb (0.1540 kW/kg)

Armament

See also

Related lists

References

Citations

  1. ^ a b c Jackson 1968, p. 367.
  2. ^ a b c d Jackson 1968, p. 364
  3. ^ a b c d e Jackson 1968, p. 365
  4. ^ a b Taylor 1969, p. 322
  5. ^ Jackson 1968, pp. 365–366
  6. ^ a b c d e Jackson 1968, p. 366
  7. ^ a b Thetford 1978, p. 55
  8. ^ Jackson 1968, p. 370
  9. ^ Jackson 1968, p. 368
  10. ^ Jackson 1968, pp. 367–369
  11. ^ Mason 1994, p. 243.
  12. ^ Jackson 1968, p. 371
  13. ^ Jackson 1968, p. 369
  14. ^ Jackson 1968, pp. 371–372
  15. ^ a b c Jackson 1968, p. 372
  16. ^ Shores, Cull & Izawa 1992, pp. 276, 337–338, 340
  17. ^ Jackson 1968, pp. 372–374
  18. ^ a b c Jackson 1968, p. 374
  19. ^ Jackson 1968, pp. 374–376
  20. ^ Jackson 1968, p. 377
  21. ^ Molson & Taylor 1982, p. 110
  22. ^ a b c d e f Kostenuk & Griffin 1977, p. 255
  23. ^ Thetford 1978, p. 53.
  24. ^ Mason 1994, p. 242

Bibliography

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