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Westland Welkin

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Title: Westland Welkin  
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Subject: Westland aircraft, Vickers Type 432, Westland Helicopters, Westland Whirlwind (fighter), Rolls-Royce Merlin
Collection: British Fighter Aircraft 1940–1949, Westland Aircraft
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Westland Welkin

Westland Welkin
Welkin Mk I DX282
Role high altitude fighter
Manufacturer Westland Aircraft
Designer W.E.W. Petter
First flight 1 November 1942
Introduction May 1944
Retired November 1944
Primary user Royal Air Force
Number built 75 + 2 prototypes + 26 engine-less airframes

The Westland Welkin was a British twin-engine heavy fighter from the Westland Aircraft Company, designed to fight at extremely high altitudes, in the stratosphere; the word welkin meaning "the vault of heaven" or the upper atmosphere.[1][2] First conceived in 1940, it was built from 1942–43 in response to the arrival of modified Junkers Ju 86P bombers flying reconnaissance missions[3] that suggested the Luftwaffe might attempt to re-open the bombing of England from high altitude. The threat never materialised; consequently, Westland produced only a small number of Welkins and few of these flew.


  • Design and development 1
  • Operational history 2
  • Variants 3
  • Operators 4
  • Specifications (Welkin F.Mk.I) 5
  • See also 6
  • References 7
    • Notes 7.1
    • Bibliography 7.2
  • External links 8

Design and development

Westland put forward their P.14, essentially an adaptation of Westland's Whirlwind fighter layout (and a more experimental twin, the P.13) to meet Air Ministry Specification F.4 of 1940 for a high altitude fighter.[4] The most obvious feature was the enormous high aspect ratio wing, with a span on the production aircraft of 70 feet (21 m).[5] The compact but troublesome Rolls-Royce Peregrine engines of the Whirlwind were replaced by the more powerful two-stage Rolls Royce Merlin Mk.76/77. However, the most significant feature was a pressurised cockpit. The last item required the majority of the effort in designing what would become the Welkin. After extensive development a new cockpit was developed that was built out of heavy-gauge duraluminium bolted directly to the front of the main spar. The cockpit hood used an internal layer of thick perspex to hold the pressure, and an outer thin layer to form a smooth line. Heated air was blown between the two to keep the canopy clear of frost.

In January 1941, the Ministry of Aircraft Production authorised the building of two P.14 prototypes. The F.4/40 specification was revised into F.7/41 that year. The Welkin design was now in competition with the Vickers Type 432 with Merlin 61 engines.

The pressurisation system was driven by a Rotol supercharger attached to the left-hand engine (this was the difference between the Merlin 76 and 77), providing a constant pressure of 3.5 psi (24 kPa) over the exterior pressure. This resulted in an apparent cabin altitude of 24,000 feet (7,300 m) when the aircraft was operating at its design altitude of 45,000 ft (14,000 m). This cabin altitude was still too high for normal breathing, so the pilot had to wear an oxygen mask during flight. A rubber gasket filled with the pressurized air sealed the canopy when the system was turned on, and a valve ensured the pressure was controlled automatically. Moreover, the pilot also had to wear a high altitude suit as he might have been required to bail out at altitude.

The Welkin required a sophisticated electrical system. This was to minimise the number of seals and points of entry in the cockpit for the controls and instrumentation. It took an electrician experienced in the features of the Welkin four hours to undertake a pre-flight check of this system. The wings were so large that the high lift Fowler flaps of the Whirlwind were not needed, and were replaced by a simple split flap. The extra wing area also required more stability, so the tail was lengthened to provide a longer moment arm. The armament − four Hispano 20 mm cannon − was the same as the Whirlwind's, but the Welkin carried the guns in a tray in its belly, which facilitated loading. In that position, muzzle flash was also less likely to dazzle the pilot.

Operational history

Welkin Mk I, emphasising the great span of the high-aspect ratio wings.

By the time the Welkin Mk.I was complete and in production, it was apparent that the Luftwaffe was no longer conducting high altitude missions, due largely to successful interceptions by specially modified Supermarine Spitfires. Only 77 complete Welkins were produced, plus a further 26 as engine-less airframes.[6] Two Welkins served with the Fighter Interception Unit based at RAF Wittering from May to November 1944, where they were used to gain experience and formulate tactics for high altitude fighter operations. A two-seat, radar-equipped night fighter version known as the Welkin NF.Mk.II for specification F.9/43 was developed but only one was eventually produced as the variant was not ordered into production.[7][8]

Information on the Welkin was only released at the end of the war.[9]

The Welkin was seriously handicapped by compressibility problems exacerbated by its long but thick wings, causing the flight envelope (flyable speed range) between high-incidence stall and shock-stall to become very small at high altitudes - any decrease in airspeed causing a "normal" stall, any increase causing a shock-stall due to the aircraft's limiting critical Mach number. This reduction of the speed envelope is a problem common to all subsonic, high altitude designs and also occurred with the later Lockheed U-2. When W.E.W. Petter came to design his next high altitude aircraft, the English Electric Canberra jet bomber, it was distinguished by noticeably short wings.


  • Welkin Mk.I : Single-seat twin-engine high altitude fighter aircraft.
  • Welkin NF.Mk.II : Two-seat night fighter prototype.


United Kingdom

Specifications (Welkin F.Mk.I)

Data from [10][11]

General characteristics
  • Crew: One pilot
  • Length: 41 ft 6 in (12.67 m)
  • Wingspan: 70 ft 0 in (21.30 m)
  • Height: 15 ft 9 in (4.80 m)
  • Wing area: 250 ft2 (23 m2)
  • Empty weight: 8,310 lb (3,768 kg)
  • Loaded weight: 10,356 lb (4,697 kg)
  • Max. takeoff weight: 11,410 lb (5,175 kg)
  • Powerplant: 2 × Rolls-Royce Merlin 76/77 liquid-cooled piston engine, 1,233 hp (920 kW) each



See also

Related development
Aircraft of comparable role, configuration and era
Related lists



  1. ^ "Welkin. (n.d.)." Web, The American Heritage Dictionary of the English Language, Fourth Edition. Retrieved: 20 July 2009.
  2. ^ "welkin, n.". OED Online. September 2013. Oxford University Press. (accessed 13 September 2013).
  3. ^ Velek, Ovčáčík & Susa 2005, p. 1.
  4. ^ Buttler 2004, p. 47.
  5. ^ For comparison, the Avro Lancaster four-engined heavy bomber had a span of 102 feet (31 m) and the de Havilland Mosquito twin-engined light bomber and fighter had a 54-foot (16 m) span.
  6. ^ Velek, Ovčáčík & Susa 2005, p. 3.
  7. ^ Buttler 2004, p. 48.
  8. ^ Velek, Ovčáčík & Susa 2005, pp. 13–14.
  9. ^ June 2Ist, 1945 "New Aircraft Types"Flight
  10. ^ a b .jaapteeuwen.comWestland Welkin on Retrieved: 23 July 2009.
  11. ^ a b Green & Swanborough 1981, p. 60.


  • Buttler, T. (2004). British Secret Projects: Fighters and Bombers 1935–1950. Hinckley, UK: Midland.  
  • Goulding, James and Robert Jones. "Meteor, Whirlwind and Welkin". Camouflage and Markings: RAF Fighter Command Northern Europe, 1936–45. London: Ducimus Books, 1971. ISBN 0-903234-00-9.
  • Green, W.; Swanborough, G. (1981). RAF Fighters, Part 3 (WW2 Aircraft Fact Files). London: Jane's Publishing.  
  • James, Derek N. Westland: A History. Gloucestershire UK: Tempus Publishing Ltd., 2002. ISBN 0-7524-2772-5.
  • Mondey, David. Westland (Planemakers 2). London: Jane's Publishing Company, 1982. ISBN 0-7106-0134-4.
  • Velek, M.; Ovčáčík, M.; Susa, K (2005). Westland Welkin F Mk.1, NF Mk.II. Prague, Czech Republic: Mark I Ltd.  
  • Webb, D. Collier. "Tested & Failed, Flight Test Accidents of the 1940s-1960s: Westland Welkin." Aeroplane Monthly, February 1996.

External links

  • British Aircraft of WW2 dead link
  • British Aircraft Directory entry dead link
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