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558:, the FD2's engine manufacturer, also dismissed the attempt, claiming that the air intakes were unsuitable for speeds around Mach 1.5, and that the Avon engine would disintegrate at such speeds, despite an absence of any practical data to support this assertion. In spite of this opposition, Fairey sought to continue, and were given permission to proceed. The Ministry provided no financial support, having opted instead to loan the aircraft itself to Fairey and to charge the firm for its use of RAE assets. Fairey also had to finance its own insurance. Regardless, Fairey chose to continue with the record attempt.
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upwards giving a noticeable bulge on the wing upper surface. No attempt was made to fit variable intakes. At high throttle settings, considerable suction into the inlets was generated; in the event of a sudden down-throttle motion by the pilot would result in air "spilling" out of the intakes, which was a concern because it could flow above the wing and disrupt the vortex. Small lips were added to the intakes to help prevent this, but this proved to cause intake buzzing. Changes to the ducts, assisted by Rolls-Royce, addressed this issue.
808:. Although high-speed performance appeared to be predictable, a dedicated testbed aircraft was desired, especially for drag measurements. As early as 1958, the RAE and Fairey began discussions about converting one of the Delta 2 prototypes to support the ogee wing. Fairey proposed stretching the fuselage a further three feet to better match the long planform, with the wing extending out onto the drooping nose. However, calculations showed that this extension was not great enough to counter the forward moving
687:, which called for a two-seat fighter equipped with radar and missiles with suitable performance to achieve an altitude of 60,000 feet (18,000 m) and Mach 2 within six minutes of taking off; while the company thought that their design would be fully capable of meeting the specified requirements, it was believed that the complete weapon system would not be fully developed until 1962. Thus, Fairey proposed that a simpler interim aircraft, if selected, could be available by 1960 or potentially earlier.
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levels of performance; however, speeds of Mach 1.6 were attained during its test flights. In total, the BAC 221 featured a new wing, engine inlet configuration, a Rolls-Royce Avon RA.28, modified vertical stabilizer and a lengthened undercarriage to mimic
Concorde's attitude on the ground. It first flew on 1 May 1964. The sole 221 was used for varied flight testing from 1964 until 1973, after which it was placed on public display.
331:. In February 1949, it was suggested that Fairey examine the prospects for a single-engine transonic aircraft as an alternative; by the end of the year, the company had produced their new project, out of which the Fairey Delta 2 (FD2) would directly originate. Accordingly, the Ministry issued Air Ministry Specification ER.103 for the project, ordering that a pair of prototype aircraft be produced.
471:
602:, raising it to 1,132 mph (1,811 km/h) or Mach 1.73. This achievement exceeded the prior recorded airspeed record by 310 mph, or 37 per cent; never before had the record ever been raised by such a margin. The achievement had also made the Fairey Delta 2 the first jet aircraft to exceed 1,000 mph (1,600 km/h) in level flight.
763:, Fairey joined forces with Rolls-Royce and Dassault in a collaborative effort to produce a delta wing aircraft capable of reaching Mach 2 to meet the German demand for fighter aircraft. The proposal would have seen Dassault produce the wings, Fairey manufacture the fuselage, and Rolls-Royce provide the engine, which was intended to be a
789:
increases lift by an amount known as vortex lift. The wing root chord should be as long as possible, and highly swept where it meets the forward fuselage. Continued studies of this basic concept led to the ogee layout and it eventually became apparent that a series of full-scale flight tests would be necessary for its validation.
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514:, France; a detachment of Dassault engineers closely observed these trials, learning a great deal about delta wing aircraft from the FD2. Dassault went on to produce the MD.550 Mystère-Delta design, which Wood notes "bore a striking resemblance" to the FD2; the MD.550 design would proceed to be manufactured as the successful
31:
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or ogival delta design. This design aimed to improve both supersonic wave drag with high leading-edge sweep and low thickness/chord ratio at the root, and low-speed lift through flow separation at the leading edge which creates a rolled up vortex on top of the wing. The added suction under the vortex
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for calibration purposes were also conducted by the RAF. Operational demands on both the pilot and ground crews were severe and many runs were attempted but failed to qualify on one technicality or another. On the final day available, the first run also failed; the second and last run that day became
605:
News of the new airspeed record quickly spread and had a prompt impact upon the international aeronautics industry, typical reactions being shock and near-disbelief. According to Wood, consequences included in-depth studies of the FD2 airframe by the United States and the major reshaping of military
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The Delta 2 has a relatively small cockpit for the pilot which left little room for the installation of additional equipment. The Delta was the first
British aircraft to fly using all-powered controls. These controls, designed and produced by Fairey, were fully duplicated. The flight control system
547:. Fairey had great difficulty in obtaining permission for the attempt. Twiss stated that the situation was "curiously inverted" from expectations, having expected that government agencies would have been enthusiastically pressing for a record-breaking flight as a means to bolster national prestige.
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since the testing schedule did not yet require its use at that time. According to Wood, many members of the development team recognised that the FD2 possessed huge speed potential, beyond any other
British-built aircraft in existence of that time. During early flight testing, Twiss came to realise
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were received. Tests of the Delta 2's low-level supersonic flight capability were disrupted due to the perceived heightened risk posed by supersonic booms being produced during lower altitude flight; as such, the
Ministry of Supply refused to allow this testing to be performed over the UK. Despite
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Once the manufacturer's testing was completed, both aircraft were formally handed over to the RAE. In addition to providing the institution with useful information on the characteristics of the 60°-swept delta wing, from 1958 onwards, the FD2 aircraft participated in various research projects and
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so that the tests could be performed. The French government required the tests to be insured against damage claims; this demand had proved unacceptable with two
British insurance companies quoting a premium of about £1,000 per flight; however, a French company insured them for £40. No claims were
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One major advantage of the new design was its larger fuel capacity, which has been a major problem for the original FD2. The Delta 2 had often run low on fuel while still accelerating, thereby never reaching its full performance. The modifications for the 221 meant it was not capable of the same
440:
on its 14th flight when internal pressure build-up collapsed the fuselage collector tank, closing off the fuel supply to the engine, while heading away from the airfield at 30,000 ft (9,100 m), 30 mi (50 km) after taking off from RAF Boscombe Down. Twiss managed to glide to a
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fluid, which required a larger reservoir to hold it, a higher capacity pump to move it quickly enough through the system, and so on through the hydraulic system. Moving the intakes below the wing meant they were no longer in-line with the compressor face so the ducting to the engine was curved
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In order to reduce the risk of another competitor beating them to it, preparations had to be carried out in a short space of time and in great secrecy. The development and deployment of equipment suitable for the accurate measurement of flight at such speeds was a challenge in itself. For this
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was promptly recruited as Fairey's new Chief
Engineer and became a major force behind the programme. Data that had been obtained from the earlier model work also proved to have been highly valuable to the Fairy Delta 2 programme. Early development work on the FD2 would be hindered by two major
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was hydraulically operated and possessed no mechanical backup. Fairey had recently developed a new high-pressure hydraulic system and this was used in the design. The hydraulics provided no feedback or "feel" to the pilot's controls, so another system providing artificial feel was necessary.
293:(RAF) had developed an intense desire to advance the performance of their aircraft; in particular, the service sought new fighter aircraft that would be capable of routinely flying at very high speeds and high altitudes as a long-term replacement for its existing inventory of roughly 700
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aircraft programs in France. Fairey itself was elated with the achievement, viewing it as a practical endorsement of their design, and fuelled the firm's ambitions to establish a family of supersonic fighters on its basis. The record stood until 12 December 1957, when it was beaten by a
389:. In addition to seeking very high performance, the design adopted a general configuration and structure that would be readily adapted to future military requirements, so that it could potentially become a fighter aircraft. In total, a pair of flight-capable aircraft were produced:
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that had influenced German decision makers, and the F-104G was selected instead. This was the end for the FD2 as a fighter concept; the concept never saw any use as a production aircraft; Wood summarised the state of affairs as "the harvest was left to France to gather".
848:, were adopted by BAC in order to not overrun on the fixed-price contract it had been issued for the work; some engineers were allegedly frustrated by this as apparent means of further improvement were dismissed. On 7 July 1961, the newly christened
384:
In
September 1952, technical drawings of the Fairey Delta 2 were issued and the development proper commenced. From the project's beginning, Fairey designed the parameters of the FD2 to intentionally exceed that which was necessary only to achieving
305:
aerodynamics, structures and aero engines by the
British aircraft industry had the effect of increasing demand and the potential capabilities of new fighters. In addition to developing improved versions of existing and emerging fighters such as the
526:. The substantial rebuilding of the aircraft to participate in further research was first mooted in that same year as well. In its original configuration, the Delta 2 performed flight tests, interspersed with periods of storage, up until mid-1966.
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of 1,132 mph (1,822 km/h), exceeding the previous official record by 310 mph (500 km/h). The Delta 2 held the absolute World Air Speed Record for over a year. It continued to be used for flight testing, and was allocated to the
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stabilization system, and have the engine intakes moved under the wing. The minimal conversion was considered to be more of a 'compromise', being less slender and lacking the additional fuel capacity that the maximal option provided for.
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According to Fairey's projections, the ER.103/B could have been ready to fly within eighteen months of having received an order, while the ER.103/C could reach the same readiness within 30 months. In particular, Fairey pursued
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at high speed on the airfield. Only the nose gear had deployed, and the aircraft sustained damage that put it out of action for eight months. Twiss, who was shaken up by the experience but otherwise uninjured, received the
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that the Delta 2 would be capable of speeds above 1,000 miles per hour (1,600 km/h) and proposed that it be flown on with the aim of breaking the current air speed record, which had then been held since 1955 by a
482:, the second Delta 2, performed its maiden flight from RAF Boscombe Down; piloted by Twiss, the aircraft reached transonic speeds during this first flight. Following the final contractor check flight on 14 April 1956,
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was formally accepted, upon which it was assigned to the RAE's high-speed research programme, conducting measurement, stability and handling research. In
September 1956, both aircraft performed flight displays at the
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twin-engine aircraft; however, the
Ministry lacked enthusiasm for the twin-engine configuration, largely due to an existing rival project underway to produce a twin-engine supersonic aircraft – this would become the
827:(BAC). Bristol suggested two ways forward, a minimal conversion with a sub-optimal wing but no other major changes, or a "maximal" conversion with a larger six foot extension to the fuselage and a much taller
321:
investigations. However, Fairey did not find this proposal attractive, believing that a piloted aircraft would be mandatory if the project was to produce any worthwhile data. Fairey commenced work on a highly
938:, making the Delta 2's wing one of the thinnest known at that time. The internal space housed both the main undercarriage and a total of four fuel tanks without any bulges or fairings in the wing, while four
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was flown to Bristol's Filton facility. Following a period of detailed design work, the re-manufacturing process commenced in April 1961. Considerable cost-cutting measures and management strategies, such as
412:
system was not incorporated. There were also a few differences in terms of equipment and instrumentation. In addition to the two flying aircraft, a single static test airframe was also completed.
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640:, was also proposed, upon which the wings would have been scaled up by 50 per cent, with no radical aerodynamic alterations made. Combat equipment would have been provisioned, including a
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On 1 April 1957, Fairey were informed by officials within the Ministry of Supply that their proposals were the favourite to meet Operational Requirement F.155. However, on 4 April 1957,
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254:. The Ministry, being interested in these proposals, issued orders for models to test the envisioned delta wing, the first of which being built in 1947; testing was performed by the
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was fitted; the nose section, including the cockpit, could be drooped 10° using a hydraulically-actuated mechanism, in a similar manner to that which was used later on Concorde.
709:, separate from the turbojet engine's fuel storage. It featured a two-man crew, a pilot and radar operator/navigation, seated in a side-by-side configuration. The fuselage was
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Fairey produced a number of proposals which would have involved the further development of the Delta 2. The first of these was another experimental aircraft, designated as the
453:
During early flight tests, repeated supersonic test runs over southern Britain were conducted; as a result of these flights, a number of claims for damages against the
554:, to the extent that it appeared that the government were opposing the endeavor. The Ministry of Supply sought to avoid any association with a speed record bid while
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nose. A long nose would normally have obscured the pilot's forward vision during landing, take-off and movement on the ground; so, to provide adequate visibility a
297:. At the time, there was a perception that Britain was trailing behind in supersonic aircraft design, and there was pressure to correct this. Events such as the
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engine with reheat; Belgium also played a role in the programme. However, the American lobby proved to be too strong, in part due to the subsequently uncovered
543:. However, Fairey found the Ministry of Supply unsupportive, having adopted the prevailing belief being that manned military aircraft would soon be replaced by
628:, which would have paired the wings of the FD2 with a revised fuselage, which had a greater span and length. The ER.103/B was to have been powered by either a
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217:. On 1 May 1964, the modified aircraft performed its first flight. The FD2 was also used as the basis for Fairey's submissions to the Ministry for advanced
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WG774 with the original polished-metal finish. It later received yellow stripes, followed by a purple and yellow scheme, before conversion to the BAC 221
812:(CoP) that resulted from the extended planform, and there were also concerns that the over-wing engine intakes would swallow the vortex above the wing.
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air-to-air missiles. Further design revisions saw the single Gyron engine being replaced by a pair of RB.122 engines instead and the adoption of the
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fighter. Wood credits the Delta 2 as having served to confirm Dassault's theories and supporting the designing and development of the Mirage III.
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missile, alongside refinements such as intake improvements and increased internal fuel capacity. Fairey stated that the aircraft was suited to
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The Fairey Delta 2 was the first jet aircraft to exceed 1,000 miles per hour (1,600 km/h) in level flight. On 10 March 1956, it set a new
1933:
Jackson, Robert. "Combat Aircraft Prototypes since 1945." Arco/Prentice Hall Press, New York, 1986. Library of Congress card number 85-18725.
495:. The Delta 2 was typically used to conduct a multitude of tests including aerodynamics characteristics, handling, and stability performance.
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1969:
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A Case Study By Aerospatiale And British Aerospace On The Concorde By Jean Rich and Clive S.Leyman,AIAA Professional Study Series,p.3-4
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432:. According to aviation author Derek Wood, the Delta 2 "proved to be an exceptional aeroplane from the outset". On 17 November 1954,
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Following on from the Delta 1, the Ministry of Supply requested that Fairey conduct a further model programme for the purpose of
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190:; two aircraft would be produced. The Delta 2 was the final aircraft to be produced by Fairey as an independent manufacturer.
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655:. Fairey claimed that the ER.103/C would be capable of attaining Mach 2.26 at an altitude of 55,000 feet (17,000 m).
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with only one reheat setting, later replaced with an RA.28 as used for speed record , 10,000 lbf (44 kN) thrust
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was completed. Various problems were encountered during the conversion. The newly lengthened landing gear required more
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In early September 1960, it was agreed that the "maximal" conversion would proceed; on 5 September of that year,
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A final attempt was made to progress a Delta 2 derivative into production came during the late 1950s for the new
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450:. One result of the crash was a temporary halt on the test programme, which did not resume until August 1955.
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In addition to the Gyron engine of earlier proposals, the proposed fighter was to be equipped with a pair of
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Testing of the Delta 2 was carried out in France for some time, in part due to Fairey's good relations with
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Far exceeded both the official 1955 record of 822.1 mph (1,323.0 km/h) by the "C" variant of a
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368:; the design team lacked experience with high speed projects. As a remedy to this, in October 1951, Sir
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and the secret 1947 record (by 241 mph (388 km/h)) of 891 mph (1,434 km/h) by the
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and would have accommodated underwing fuel tanks for extended endurance. A combat fighter model, the
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506:. In October and November 1956, a total of 47 low-level supersonic test flights were conducted from
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660:"If it were not for the clumsy way in which you tackle things in Britain, you could have made the
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technology and proceeded to submit multiple submissions based on the delta wing concept to the
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A testbed aircraft was required to verify design calculations and wind tunnel results for the
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823:. Accordingly, in July 1960, the programme moved to Bristol and was now a part of the larger
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design used a then-new type of delta wing that was being developed at the RAE known as the
258:(RAE). The program was succeeded multiple times, including an investigation into potential
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more typical of the type expected on the Concorde. Both would also be equipped with a new
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flying trials, including an investigation into the performance of ejector-type propulsive
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factors, a lack of available information on wing and intake design, and the declaring of
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According to Wood, Fairey was confronted by a combination of scepticism and apathy from
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operations, leading to further flight tests of the delta wing models to be conducted in
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980:, in BAC 221 form, is now on display alongside the British Concorde prototype at the
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During 1960, further development activity was disrupted by the purchase of Fairey by
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for a specialised aircraft for conducting investigations into flight and control at
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were adopted. As specified, the fighter was tentatively armed with wingtip-mounted
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The wing features a 60° sweep of the leading edge and was very thin, at only 4%
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as a 'super-priority' by the British government, which had necessitated delays.
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2043:"Analysis of Flight and Tunnel Tests on the Fairey Delta 2 Research Aircraft."
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At the time, Fairey was mostly known for producing naval aircraft, such as the
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During August 1955, the Delta 2 flew at supersonic speed without using its
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X-Planes of Europe: Secret Research Aircraft from the Golden Age 1946-1974
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using its 'droop snoot', described by its inventor as a sectional fuselage
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was issued for a full-scale piloted delta wing aircraft, resulting in the
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provided for significant structural strength. The sizable horn-balanced
919:, which closely fitted the Avon engine, and smoothly flowed into a long
701:(HTP) fuel for the rocket engines was stored in tanks held in underwing
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1896:
Buttler, Tony. "Fairey's Famous Research Deltas, Part Two - Type 221".
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314:, there was an appetite for even more promising entirely new aircraft.
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1946:
Faster, Further, Higher: Leading-edge Aviation Technology Since 1945.
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578:, various ground markers were installed at specified locations, and
213:" wing design so one of the aircraft was extensively rebuilt as the
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https://reports.aerade.cranfield.ac.uk/handle/1826.2/3017?show=full
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Low-speed testing of the concept was already being provided by the
2223:
1045:
1037:
957:
901:
868:
792:
791:
579:
560:
469:
333:
267:
458:
this refusal, Fairey was able to base the Delta 2 temporarily in
2007:
Concept Aircraft: Prototypes, X-Planes and Experimental Aircraft
800:. The forward wing extension and curved leading edge can be seen
785:
570:
purpose, a variety of ground measurement cameras were set up at
259:
3686:
2538:
2227:
2076:
30:
246:, a British aircraft manufacturer, had become interested in
229:; however, the FD3 never got past the drawing-board stage.
565:
The first Fairey Delta 2 (s/n WG774) in flight, circa 1956
819:, who assigned further work on the conversion project to
697:
that were mounted in fairings on the rear fuselage. The
896:
which were blended into the wing roots and featured an
900:-type nozzle. Located just forward of the nozzle were
404:, the second to be manufactured, was very similar to
1251:"Individual History: Fairey FD-2 Delta WG777/7986M."
759:. Running against a competing American bid with the
448:
Queen's Commendation for Valuable Service in the Air
4408:
4325:
4252:
4067:
3988:
3954:
3916:
3846:
3787:
3724:
3639:
3609:
3588:
3537:
3486:
3450:
3404:
3383:
3334:
3243:
3236:
2651:
2573:
2488:
2262:
2188:
2142:
2111:
1179:
Aircraft of comparable role, configuration, and era
873:
Head-on view of an FD2 on static display, June 2016
595:the only chance left before the attempt would end.
289:Meanwhile, throughout the early and mid 1950s, the
120:
112:
104:
99:
91:
81:
73:
61:
53:
45:
40:
23:
1539:
1537:
1050:Forward view of the Delta 2. Note the drooped nose
950:gave the Delta 2 a high level of manoeuvrability.
1972:(Part Work 1982–1985)." Orbis Publishing, 1985.
1389:https://patents.google.com/patent/US2736523A/en
1246:
1244:
1242:
1240:
1238:
1236:
1234:
1134:1,300 mph (2,092 km/h, 1,100 kn)
658:
598:On 10 March 1956, the Fairey Delta 2 broke the
424:, the first FD2 to be completed, conducted its
3698:
2550:
2239:
2088:
2068:Britain’s Missed Mirage? - The Fairey Delta 2
1914:. Manchester, UK: Hikoki Publications, 2012.
1765:
1763:
1750:
1748:
1746:
1744:
1742:
1740:
1515:
1513:
1511:
1509:
1507:
1505:
1486:
1484:
1399:
1397:
1328:
1326:
1324:
1322:
1320:
1318:
8:
1848:Rolls-Royce Aero Engines, Bill Gunston 1989,
881:delta monoplane. It was powered by a single
2009:. Rochester, Kent, UK: Grange Books, 2005.
1925:"BAC.211: Slender-delta Research Aircraft."
3705:
3691:
3683:
3240:
2557:
2543:
2535:
2246:
2232:
2224:
2095:
2081:
2073:
1900:, No. 94, July–August 2001, pp. 2–6.
1661:
1659:
1657:
1655:
1627:
1625:
1597:
1595:
1593:
1591:
1589:
1587:
1585:
1566:
1564:
1474:
1472:
1470:
1468:
1413:
1411:
1409:
1366:
1364:
467:ever received in either France or Norway.
182:. On 6 October 1954, the Delta 2 made its
20:
16:1950s British supersonic research aircraft
2024:. Macdonald and Jane's Publishers, 1975.
1801:
1799:
1362:
1360:
1358:
1356:
1354:
1352:
1350:
1348:
1346:
1344:
1299:
1297:
1278:
1276:
1140:830 mi (1,336 km, 720 nmi)
342:in its original design format landing at
1910:Buttler, Tony and Jean-Louis Delezenne.
1458:
1456:
1454:
1452:
1450:
1058:The Illustrated Encyclopedia of Aircraft
1963:Jane's All The World's Aircraft 1965–66
1868:
1230:
282:, which conducted its maiden flight at
150:within Fairey) is a British supersonic
1965:. London: Sampsom Low, Marston, 1965.
1079:51 ft 7.5 in (15.74 m)
221:designs, culminating in the proposed
7:
1970:Illustrated Encyclopedia of Aircraft
301:and rapid advances in the fields of
4464:1950s British experimental aircraft
1806:"British Aircraft Corporation 221."
1391:, "Sectional fuselage for aircraft"
1085:26 ft 10 in (8.18 m)
4023:de Havilland Canada DHC-1 Chipmunk
3716:manufactured in Britain since the
2104:British Aircraft Corporation (BAC)
1097:360 sq ft (33.44 m)
1091:11 ft 0 in (3.35 m)
877:The Fairey Delta 2 has a mid-wing
530:Breaking the world airspeed record
276:Air Ministry Specification E.10/47
14:
1930:, 23 July 1964, pp. 133–138.
1042:Close-up rear view of the Delta 2
4179:Rolls-Royce Thrust Measuring Rig
1877:North American F-100 Super Sabre
1013:
646:aircraft interception radar 1495
610:of the United States Air Force.
541:North American F-100 Super Sabre
29:
2618:Bristol Gordon England biplanes
2045:Her Majesty's Stationery Office
1816:Royal Navy Fleet Air Arm Museum
1204:Mikoyan-Gurevich MiG-21I Analog
1034:Specifications (Fairey Delta 2)
35:World speed record holder WG774
4307:Scottish Aviation Twin Pioneer
1818:, Retrieved: 13 December 2016.
1338:, Retrieved: 13 December 2016.
1256:, Retrieved: 13 December 2016.
1109:13,884 lb (6,298 kg)
1103:11,000 lb (4,990 kg)
1:
4134:Fairey Ultra-light Helicopter
1994:. London: Grub Street, 2000.
1215:List of experimental aircraft
729:duties at various altitudes,
685:Operational Requirement F.155
620:Operational Requirement F.155
428:, flown by Fairey test pilot
295:first-generation jet fighters
186:, flown by Fairey test pilot
4474:Aircraft first flown in 1954
4469:Tailless delta-wing aircraft
2613:Bristol Coanda monoplanes
1544:"50 years ago: 16 Mar 1956."
1028:Royal Aircraft Establishment
825:British Aircraft Corporation
582:tracking from RNAS Ford and
256:Royal Aircraft Establishment
200:Royal Aircraft Establishment
174:speeds. Features included a
86:Royal Aircraft Establishment
49:high-speed research aircraft
4038:British Aerospace Jetstream
761:Lockheed F-104G Starfighter
737:missions were also mooted.
552:Her Majesty's Civil Service
346:in 1956 during that year's
4490:
4262:Armstrong Whitworth Argosy
4079:Armstrong Whitworth A.W.52
3958: / anti-submarine
3749:English Electric Lightning
1977:Fairey Aircraft since 1915
1610:Taylor, 1984, pp. 431–433.
617:
329:English Electric Lightning
4302:Scottish Aviation Pioneer
4244:Youngman-Baynes High Lift
3936:English Electric Canberra
3417:Bristol Coanda Monoplanes
1435:Taylor 1984, pp. 430–431.
1161:Aerospatiale-BAC Concorde
769:Lockheed bribery scandals
154:that was produced by the
28:
3808:de Havilland Sea Vampire
2608:Bristol Prier monoplanes
1979:. London: Putnam, 1974.
892:. The engine was fed by
713:while large rectangular
608:McDonnell JF-101A Voodoo
4292:Hawker Siddeley Andover
3890:Hawker Siddeley Harrier
3803:de Havilland Sea Hornet
3652:George Henry Challenger
1811:13 January 2017 at the
1117:Rolls-Royce Avon RA.14R
1064:General characteristics
883:Rolls-Royce Avon RA.14R
650:de Havilland Firestreak
242:During the late 1940s,
219:all-weather interceptor
156:Fairey Aviation Company
68:Fairey Aviation Company
4164:Hawker Siddeley P.1127
4033:Handley Page Jetstream
3980:Hawker Siddeley Nimrod
3818:de Havilland Sea Vixen
3813:de Havilland Sea Venom
2593:Bristol Racing Biplane
2470:Ultra-light Helicopter
2059:"The Fairey Delta 2."
1692:Wood 1975, pp. 86, 88.
1619:Wood 1975, pp. 79, 82.
1336:Royal Air Force Museum
1254:Royal Air Force Museum
1151:Flight airspeed record
1051:
1043:
996:Royal Air Force Museum
994:, is preserved at the
973:
967:Royal Air Force Museum
874:
801:
705:and within the wing's
666:
600:World Air Speed Record
566:
475:
351:
146:(internal designation
4340:AgustaWestland Merlin
4335:AgustaWestland Apache
4287:Handley Page Hastings
2504:Avions Fairey Belfair
1722:Jarrett 2002, p. 179.
1674:Wood 1975, pp. 87–88.
1649:Wood 1975, pp. 82–83.
1640:Wood 1975, pp. 86–87.
1579:Wood 1975, pp. 78–79.
1558:Wood 1975, pp. 77–78.
1490:Wood 1975, pp. 85–86.
1444:Jackson 1986, p. 104.
1426:Wood 1975, pp. 76–77.
1403:Wood 1975, pp. 75–76.
1379:Wood 1975, pp. 71–72.
1291:Wood 1975, pp. 73–74.
1049:
1041:
961:
936:thickness-chord ratio
872:
795:
735:aerial reconnaissance
564:
478:On 15 February 1956,
473:
408:except the underwing
337:
4428:Slingsby Grasshopper
4018:Boulton Paul Balliol
3838:Supermarine Scimitar
3833:Supermarine Attacker
3739:de Havilland Vampire
3437:Bolingbroke IVT/IVTT
3335:Passenger Transports
2499:Avions Fairey Junior
2345:Long-range Monoplane
2061:Flight International
2052:14 July 2007 at the
1928:Flight International
1839:Orbis 1985, p. 1695.
1793:Taylor 1965, p. 130.
1547:Flight International
1190:English Electric P1A
982:Fleet Air Arm Museum
798:Fleet Air Arm Museum
719:de Havilland Red Top
715:variable air intakes
692:de Havilland Spectre
614:Proposed derivatives
4239:Supermarine Seagull
4189:Saunders-Roe SR.A/1
4149:Handley Page HP.115
4099:Blackburn Firecrest
3941:Handley Page Victor
3895:Panavia Tornado IDS
3880:Eurofighter Typhoon
3870:Blackburn Buccaneer
3774:Panavia Tornado ADV
3754:Eurofighter Typhoon
3734:de Havilland Hornet
3662:Eric Gordon England
2430:Firefly (monoplane)
2263:Chronological order
1992:Faster than the Sun
1784:1964, pp. 135, 137.
1713:, para 6.2.1 'Lift'
1167:Related development
954:Aircraft on display
806:Handley Page HP.115
746:Minister of Defence
653:air-to-air missiles
592:de Havilland Venoms
516:Dassault Mirage III
489:Farnborough Airshow
436:suffered an engine
420:On 6 October 1954,
227:F.155 specification
41:General information
4400:Westland Whirlwind
4365:Westland Dragonfly
4282:Blackburn Beverley
4194:Saunders-Roe SR.53
4144:Handley Page HP.88
4109:Boulton Paul P.120
4104:Boulton Paul P.111
3744:de Havilland Venom
1960:Taylor, John W. R.
1734:1964, pp. 133–134.
1052:
1044:
974:
911:The Delta 2 has a
875:
810:centre of pressure
802:
699:high-test peroxide
634:Rolls-Royce RB.122
630:de Havilland Gyron
567:
502:of France and the
476:
443:dead-stick landing
352:
338:The first Delta 2
286:on 12 March 1951.
272:Woomera, Australia
252:Ministry of Supply
195:world speed record
164:Ministry of Supply
4446:
4445:
4438:Slingsby Sedbergh
4385:Westland Sea King
4360:Westland Commando
4345:Bristol Belvedere
4297:Percival Pembroke
3779:Supermarine Swift
3714:Military aircraft
3680:
3679:
3672:Archibald Russell
3635:
3634:
2598:Bristol Monoplane
2532:
2531:
2221:
2220:
2022:Project Cancelled
2005:Winchester, Jim.
1944:Jarrett, Philip.
1920:978-1-902-10921-3
1683:Wood 1975, p. 88.
1665:Wood 1975, p. 83.
1631:Wood 1975, p. 82.
1601:Wood 1975, p. 79.
1570:Wood 1975, p. 78.
1531:Wood 1975, p. 77.
1499:Wood 1975, p. 86.
1478:Wood 1975, p. 85.
1417:Wood 1975, p. 76.
1370:Wood 1975, p. 75.
1312:Wood 1975, p. 71.
1303:Wood 1975, p. 74.
1282:Wood 1975, p. 73.
965:preserved in the
817:Westland Aircraft
677:
675:Dassault Aviation
500:Dassault Aviation
284:RAF Boscombe Down
158:in response to a
152:research aircraft
136:
135:
105:Introduction date
77:On public display
4481:
4433:Slingsby Prefect
4370:Westland Gazelle
4350:Bristol Sycamore
4119:Cierva Air Horse
4043:Percival Provost
3908:
3905:Westland Wyvern
3860:BAC Strikemaster
3718:Second World War
3707:
3700:
3693:
3684:
3241:
2559:
2552:
2545:
2536:
2248:
2241:
2234:
2225:
2097:
2090:
2083:
2074:
1884:
1873:
1857:
1846:
1840:
1837:
1831:
1825:
1819:
1803:
1794:
1791:
1785:
1779:
1773:
1767:
1758:
1752:
1735:
1729:
1723:
1720:
1714:
1708:
1702:
1699:
1693:
1690:
1684:
1681:
1675:
1672:
1666:
1663:
1650:
1647:
1641:
1638:
1632:
1629:
1620:
1617:
1611:
1608:
1602:
1599:
1580:
1577:
1571:
1568:
1559:
1556:
1550:
1549:, 10 March 2006.
1541:
1532:
1529:
1523:
1517:
1500:
1497:
1491:
1488:
1479:
1476:
1463:
1460:
1445:
1442:
1436:
1433:
1427:
1424:
1418:
1415:
1404:
1401:
1392:
1386:
1380:
1377:
1371:
1368:
1339:
1330:
1313:
1310:
1304:
1301:
1292:
1289:
1283:
1280:
1271:
1263:
1257:
1248:
1127:
1066:
1019:
1017:
1016:
833:Elliott Brothers
821:Hunting Aircraft
765:Rolls-Royce Spey
753:German Air Force
678:
669:
504:French Air Force
455:supersonic booms
356:Fairey Swordfish
33:
21:
4489:
4488:
4484:
4483:
4482:
4480:
4479:
4478:
4459:Fairey aircraft
4449:
4448:
4447:
4442:
4404:
4395:Westland Wessex
4321:
4317:Vickers Valetta
4248:
4234:Supermarine 545
4229:Supermarine 508
4069:
4063:
4059:Vickers Varsity
4048:Percival Prince
4008:BAC Jet Provost
3984:
3965:Avro Shackleton
3956:Maritime patrol
3950:
3946:Vickers Valiant
3912:
3906:
3875:Bristol Brigand
3842:
3828:Hawker Sea Hawk
3823:Hawker Sea Fury
3798:BAE Sea Harrier
3783:
3759:Gloster Javelin
3720:
3711:
3681:
3676:
3631:
3605:
3584:
3533:
3482:
3446:
3432:Primary Trainer
3412:Bristol Boxkite
3400:
3379:
3330:
3286:Jupiter Fighter
3232:
2653:
2647:
2575:
2569:
2563:
2533:
2528:
2484:
2258:
2252:
2222:
2217:
2190:
2184:
2138:
2107:
2101:
2054:Wayback Machine
2039:
1893:
1888:
1887:
1874:
1870:
1865:
1860:
1847:
1843:
1838:
1834:
1826:
1822:
1813:Wayback Machine
1804:
1797:
1792:
1788:
1780:
1776:
1768:
1761:
1753:
1738:
1730:
1726:
1721:
1717:
1709:
1705:
1700:
1696:
1691:
1687:
1682:
1678:
1673:
1669:
1664:
1653:
1648:
1644:
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1635:
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1623:
1618:
1614:
1609:
1605:
1600:
1583:
1578:
1574:
1569:
1562:
1557:
1553:
1542:
1535:
1530:
1526:
1518:
1503:
1498:
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1477:
1466:
1461:
1448:
1443:
1439:
1434:
1430:
1425:
1421:
1416:
1407:
1402:
1395:
1387:
1383:
1378:
1374:
1369:
1342:
1331:
1316:
1311:
1307:
1302:
1295:
1290:
1286:
1281:
1274:
1267:Flight Magazine
1264:
1260:
1249:
1232:
1228:
1223:
1185:Dassault Mirage
1147:
1123:
1062:
1036:
1014:
1012:
1009:
956:
867:
796:BAC 221 at the
778:
680:
671:Marcel Dassault
668:
622:
616:
588:Gloster Meteors
545:guided missiles
532:
508:Cazaux Air Base
418:
374:Hawker Aircraft
312:Gloster Javelin
291:Royal Air Force
244:Fairey Aviation
240:
235:
202:(RAE) in 1958.
54:National origin
36:
17:
12:
11:
5:
4487:
4485:
4477:
4476:
4471:
4466:
4461:
4451:
4450:
4444:
4443:
4441:
4440:
4435:
4430:
4425:
4423:Slingsby Cadet
4420:
4414:
4412:
4406:
4405:
4403:
4402:
4397:
4392:
4387:
4382:
4380:Westland Scout
4377:
4372:
4367:
4362:
4357:
4352:
4347:
4342:
4337:
4331:
4329:
4323:
4322:
4320:
4319:
4314:
4309:
4304:
4299:
4294:
4289:
4284:
4279:
4274:
4269:
4264:
4258:
4256:
4250:
4249:
4247:
4246:
4241:
4236:
4231:
4226:
4221:
4216:
4211:
4206:
4201:
4196:
4191:
4186:
4181:
4176:
4171:
4166:
4161:
4156:
4151:
4146:
4141:
4136:
4131:
4129:Fairey Delta 2
4126:
4124:Fairey Delta 1
4121:
4116:
4111:
4106:
4101:
4096:
4091:
4086:
4081:
4075:
4073:
4065:
4064:
4062:
4061:
4056:
4051:
4045:
4040:
4035:
4030:
4025:
4020:
4015:
4010:
4005:
4000:
3994:
3992:
3986:
3985:
3983:
3982:
3977:
3972:
3970:Fairey Firefly
3967:
3961:
3959:
3952:
3951:
3949:
3948:
3943:
3938:
3933:
3928:
3922:
3920:
3914:
3913:
3911:
3910:
3902:
3900:SEPECAT Jaguar
3897:
3892:
3887:
3882:
3877:
3872:
3867:
3865:BAE Harrier II
3862:
3856:
3854:
3844:
3843:
3841:
3840:
3835:
3830:
3825:
3820:
3815:
3810:
3805:
3800:
3794:
3792:
3785:
3784:
3782:
3781:
3776:
3771:
3766:
3764:Gloster Meteor
3761:
3756:
3751:
3746:
3741:
3736:
3730:
3728:
3722:
3721:
3712:
3710:
3709:
3702:
3695:
3687:
3678:
3677:
3675:
3674:
3669:
3664:
3659:
3654:
3649:
3647:Frank Barnwell
3643:
3641:
3637:
3636:
3633:
3632:
3630:
3629:
3624:
3619:
3613:
3611:
3607:
3606:
3604:
3603:
3598:
3592:
3590:
3586:
3585:
3583:
3582:
3577:
3572:
3567:
3562:
3557:
3552:
3547:
3541:
3539:
3535:
3534:
3532:
3531:
3526:
3521:
3516:
3511:
3506:
3501:
3496:
3490:
3488:
3484:
3483:
3481:
3480:
3478:Superfreighter
3475:
3470:
3465:
3460:
3454:
3452:
3448:
3447:
3445:
3444:
3439:
3434:
3429:
3424:
3419:
3414:
3408:
3406:
3402:
3401:
3399:
3398:
3393:
3387:
3385:
3384:Reconnaissance
3381:
3380:
3378:
3377:
3372:
3367:
3359:
3354:
3349:
3344:
3338:
3336:
3332:
3331:
3329:
3328:
3323:
3318:
3313:
3308:
3303:
3298:
3293:
3288:
3283:
3278:
3273:
3268:
3263:
3258:
3253:
3247:
3245:
3238:
3234:
3233:
3231:
3230:
3225:
3220:
3215:
3210:
3205:
3200:
3195:
3190:
3185:
3180:
3175:
3170:
3165:
3160:
3155:
3150:
3145:
3140:
3135:
3130:
3125:
3120:
3115:
3110:
3105:
3100:
3095:
3090:
3085:
3080:
3075:
3070:
3065:
3056:
3051:
3046:
3041:
3036:
3031:
3026:
3021:
3016:
3011:
3006:
3001:
2996:
2991:
2986:
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2625:
2620:
2615:
2610:
2605:
2600:
2595:
2590:
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2579:
2577:
2574:Pre-numbering
2571:
2570:
2564:
2562:
2561:
2554:
2547:
2539:
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2526:
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2250:
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2200:
2194:
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2189:International
2186:
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2183:
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2177:
2172:
2167:
2162:
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2140:
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2108:
2102:
2100:
2099:
2092:
2085:
2077:
2071:
2070:
2065:
2056:
2038:
2037:External links
2035:
2034:
2033:
2018:
2003:
1990:Twiss, Peter.
1988:
1975:Taylor, H. A.
1973:
1966:
1957:
1948:Putnam, 2002.
1942:
1931:
1922:
1908:
1898:Air Enthusiast
1892:
1889:
1886:
1885:
1867:
1866:
1864:
1861:
1859:
1858:
1841:
1832:
1820:
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1759:
1736:
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1480:
1464:
1446:
1437:
1428:
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1381:
1372:
1340:
1314:
1305:
1293:
1284:
1272:
1258:
1229:
1227:
1224:
1222:
1219:
1218:
1217:
1206:
1205:
1202:
1197:
1192:
1187:
1176:
1175:
1173:Fairey Delta 1
1164:
1163:
1158:
1153:
1146:
1143:
1142:
1141:
1135:
1132:Maximum speed:
1121:
1120:
1110:
1104:
1098:
1092:
1086:
1080:
1074:
1035:
1032:
1031:
1030:
1024:
1023:
1021:United Kingdom
1008:
1005:
1004:
1003:
989:
955:
952:
915:cross-section
866:
863:
777:
774:
695:rocket engines
657:
615:
612:
531:
528:
417:
416:Flight testing
414:
391:Serial numbers
370:Robert Lickley
363:Fairey Firefly
280:Fairey Delta 1
239:
236:
234:
231:
223:Fairey Delta 3
140:Fairey Delta 2
134:
133:
122:
118:
117:
116:6 October 1954
114:
110:
109:
106:
102:
101:
97:
96:
93:
89:
88:
83:
79:
78:
75:
71:
70:
65:
59:
58:
57:United Kingdom
55:
51:
50:
47:
43:
42:
38:
37:
34:
26:
25:
24:Fairey Delta 2
15:
13:
10:
9:
6:
4:
3:
2:
4486:
4475:
4472:
4470:
4467:
4465:
4462:
4460:
4457:
4456:
4454:
4439:
4436:
4434:
4431:
4429:
4426:
4424:
4421:
4419:
4416:
4415:
4413:
4411:
4407:
4401:
4398:
4396:
4393:
4391:
4390:Westland Wasp
4388:
4386:
4383:
4381:
4378:
4376:
4375:Westland Lynx
4373:
4371:
4368:
4366:
4363:
4361:
4358:
4356:
4353:
4351:
4348:
4346:
4343:
4341:
4338:
4336:
4333:
4332:
4330:
4328:
4324:
4318:
4315:
4313:
4312:Short Belfast
4310:
4308:
4305:
4303:
4300:
4298:
4295:
4293:
4290:
4288:
4285:
4283:
4280:
4278:
4277:Beagle Basset
4275:
4273:
4270:
4268:
4265:
4263:
4260:
4259:
4257:
4255:
4251:
4245:
4242:
4240:
4237:
4235:
4232:
4230:
4227:
4225:
4224:Slingsby T.53
4222:
4220:
4219:Short Sperrin
4217:
4215:
4212:
4210:
4207:
4205:
4202:
4200:
4197:
4195:
4192:
4190:
4187:
4185:
4182:
4180:
4177:
4175:
4174:Hunting H.126
4172:
4170:
4167:
4165:
4162:
4160:
4159:Hawker P.1072
4157:
4155:
4154:Hawker P.1052
4152:
4150:
4147:
4145:
4142:
4140:
4139:Folland Midge
4137:
4135:
4132:
4130:
4127:
4125:
4122:
4120:
4117:
4115:
4112:
4110:
4107:
4105:
4102:
4100:
4097:
4095:
4092:
4090:
4087:
4085:
4082:
4080:
4077:
4076:
4074:
4072:
4068:Prototype and
4066:
4060:
4057:
4055:
4052:
4049:
4046:
4044:
4041:
4039:
4036:
4034:
4031:
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4026:
4024:
4021:
4019:
4016:
4014:
4011:
4009:
4006:
4004:
4001:
3999:
3996:
3995:
3993:
3991:
3987:
3981:
3978:
3976:
3975:Fairey Gannet
3973:
3971:
3968:
3966:
3963:
3962:
3960:
3957:
3953:
3947:
3944:
3942:
3939:
3937:
3934:
3932:
3929:
3927:
3924:
3923:
3921:
3919:
3915:
3909:
3903:
3901:
3898:
3896:
3893:
3891:
3888:
3886:
3885:Hawker Hunter
3883:
3881:
3878:
3876:
3873:
3871:
3868:
3866:
3863:
3861:
3858:
3857:
3855:
3853:
3852:ground attack
3849:
3845:
3839:
3836:
3834:
3831:
3829:
3826:
3824:
3821:
3819:
3816:
3814:
3811:
3809:
3806:
3804:
3801:
3799:
3796:
3795:
3793:
3790:
3786:
3780:
3777:
3775:
3772:
3770:
3769:Hawker Hunter
3767:
3765:
3762:
3760:
3757:
3755:
3752:
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3747:
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3740:
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3365:
3364:Britain First
3360:
3358:
3355:
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3348:
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3333:
3327:
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3319:
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3314:
3312:
3309:
3307:
3304:
3302:
3299:
3297:
3294:
3292:
3289:
3287:
3284:
3282:
3279:
3277:
3274:
3272:
3271:M.1 Monoplane
3269:
3267:
3264:
3262:
3259:
3257:
3254:
3252:
3249:
3248:
3246:
3242:
3239:
3235:
3229:
3226:
3224:
3221:
3219:
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3209:
3206:
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3201:
3199:
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3017:
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3007:
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2720:
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2707:
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2702:
2699:
2697:
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2687:
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2679:
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2669:
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2659:
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2650:
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2517:
2515:
2512:
2510:
2507:
2505:
2502:
2500:
2497:
2496:
2494:
2491:
2490:Avions Fairey
2487:
2481:
2478:
2476:
2473:
2471:
2468:
2466:
2463:
2461:
2458:
2456:
2453:
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2398:
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2388:
2386:
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2378:
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2373:
2371:
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2333:
2331:
2328:
2326:
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2318:
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2311:
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2306:
2303:
2301:
2298:
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2291:
2288:
2286:
2283:
2281:
2278:
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2273:
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2267:
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2261:
2256:
2249:
2244:
2242:
2237:
2235:
2230:
2229:
2226:
2214:
2211:
2209:
2206:
2204:
2201:
2199:
2196:
2195:
2193:
2187:
2181:
2178:
2176:
2173:
2171:
2168:
2166:
2163:
2161:
2158:
2156:
2153:
2151:
2148:
2147:
2145:
2141:
2135:
2132:
2130:
2127:
2125:
2122:
2120:
2117:
2116:
2114:
2110:
2105:
2098:
2093:
2091:
2086:
2084:
2079:
2078:
2075:
2069:
2066:
2064:
2062:
2057:
2055:
2051:
2048:
2046:
2041:
2040:
2036:
2031:
2030:0-356-08109-5
2027:
2023:
2020:Wood, Derek.
2019:
2016:
2015:1-84013-809-2
2012:
2008:
2004:
2001:
2000:1-902304-43-8
1997:
1993:
1989:
1986:
1985:0-370-00065-X
1982:
1978:
1974:
1971:
1967:
1964:
1961:
1958:
1955:
1954:0-851-77876-3
1951:
1947:
1943:
1940:
1939:0-671-61953-5
1936:
1932:
1929:
1926:
1923:
1921:
1917:
1913:
1909:
1907:
1903:
1899:
1895:
1894:
1890:
1882:
1878:
1872:
1869:
1862:
1855:
1854:1 85260 037 3
1851:
1845:
1842:
1836:
1833:
1830:1964, p. 136.
1829:
1824:
1821:
1817:
1814:
1810:
1807:
1802:
1800:
1796:
1790:
1787:
1783:
1778:
1775:
1772:1964, p. 135.
1771:
1766:
1764:
1760:
1757:1964, p. 134.
1756:
1751:
1749:
1747:
1745:
1743:
1741:
1737:
1733:
1728:
1725:
1719:
1716:
1712:
1707:
1704:
1698:
1695:
1689:
1686:
1680:
1677:
1671:
1668:
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1660:
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1656:
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1637:
1634:
1628:
1626:
1622:
1616:
1613:
1607:
1604:
1598:
1596:
1594:
1592:
1590:
1588:
1586:
1582:
1576:
1573:
1567:
1565:
1561:
1555:
1552:
1548:
1545:
1540:
1538:
1534:
1528:
1525:
1522:1964, p. 133.
1521:
1516:
1514:
1512:
1510:
1508:
1506:
1502:
1496:
1493:
1487:
1485:
1481:
1475:
1473:
1471:
1469:
1465:
1459:
1457:
1455:
1453:
1451:
1447:
1441:
1438:
1432:
1429:
1423:
1420:
1414:
1412:
1410:
1406:
1400:
1398:
1394:
1390:
1385:
1382:
1376:
1373:
1367:
1365:
1363:
1361:
1359:
1357:
1355:
1353:
1351:
1349:
1347:
1345:
1341:
1337:
1334:
1333:"Fairey FD2."
1329:
1327:
1325:
1323:
1321:
1319:
1315:
1309:
1306:
1300:
1298:
1294:
1288:
1285:
1279:
1277:
1273:
1270:23 March 1956
1269:
1268:
1262:
1259:
1255:
1252:
1247:
1245:
1243:
1241:
1239:
1237:
1235:
1231:
1225:
1220:
1216:
1213:
1212:
1211:
1210:
1209:Related lists
1203:
1201:
1198:
1196:
1193:
1191:
1188:
1186:
1183:
1182:
1181:
1180:
1174:
1171:
1170:
1169:
1168:
1162:
1159:
1157:
1154:
1152:
1149:
1148:
1144:
1139:
1136:
1133:
1130:
1129:
1128:
1126:
1118:
1114:
1111:
1108:
1107:Gross weight:
1105:
1102:
1101:Empty weight:
1099:
1096:
1093:
1090:
1087:
1084:
1081:
1078:
1075:
1072:
1069:
1068:
1067:
1065:
1060:
1059:
1056:
1048:
1040:
1033:
1029:
1026:
1025:
1022:
1011:
1010:
1006:
1001:
997:
993:
990:
987:
983:
979:
976:
975:
972:
968:
964:
960:
953:
951:
949:
945:
941:
937:
932:
928:
926:
922:
918:
914:
909:
907:
903:
899:
895:
891:
887:
884:
880:
871:
864:
862:
858:
855:
851:
847:
842:
837:
834:
830:
826:
822:
818:
813:
811:
807:
799:
794:
790:
787:
783:
775:
773:
770:
766:
762:
758:
754:
749:
747:
743:
742:Duncan Sandys
738:
736:
732:
728:
724:
720:
716:
712:
708:
704:
700:
696:
693:
688:
686:
679:
676:
673:, founder of
672:
665:
663:
656:
654:
651:
647:
643:
639:
635:
631:
627:
621:
613:
611:
609:
603:
601:
596:
593:
589:
586:; flights by
585:
581:
577:
573:
563:
559:
557:
553:
548:
546:
542:
537:
529:
527:
525:
519:
517:
513:
509:
505:
501:
496:
494:
490:
485:
481:
472:
468:
465:
462:and later in
461:
456:
451:
449:
444:
439:
435:
431:
427:
426:maiden flight
423:
415:
413:
411:
407:
403:
399:
395:
392:
388:
382:
380:
379:Fairey Gannet
375:
371:
367:
364:
360:
357:
349:
345:
341:
336:
332:
330:
325:
320:
315:
313:
309:
308:Hawker Hunter
304:
300:
296:
292:
287:
285:
281:
277:
273:
269:
265:
261:
257:
253:
249:
245:
237:
232:
230:
228:
224:
220:
216:
212:
208:
203:
201:
196:
191:
189:
185:
184:maiden flight
181:
177:
173:
169:
165:
161:
160:specification
157:
153:
149:
145:
141:
131:
127:
123:
119:
115:
111:
107:
103:
98:
94:
90:
87:
84:
80:
76:
72:
69:
66:
64:
60:
56:
52:
48:
44:
39:
32:
27:
22:
19:
4355:Saro Skeeter
4272:Auster AOP.9
4267:Auster AOP.6
4199:Short Seamew
4128:
4071:experimental
4054:Short Tucano
4028:Folland Gnat
3926:Avro Lincoln
3850: /
3667:Leslie Frise
3657:Henri Coandă
3528:
3487:Experimental
3363:
3266:Bristol S.2A
2654:designations
2652:Manufacturer
2514:Tipsy Nipper
2464:
2460:Jet Gyrodyne
2175:Three-Eleven
2170:Strikemaster
2133:
2060:
2044:
2021:
2006:
1991:
1976:
1962:
1945:
1927:
1911:
1897:
1891:Bibliography
1871:
1844:
1835:
1827:
1823:
1815:
1789:
1781:
1777:
1769:
1754:
1731:
1727:
1718:
1706:
1697:
1688:
1679:
1670:
1645:
1636:
1615:
1606:
1575:
1554:
1546:
1527:
1519:
1495:
1462:Twiss, 2000.
1440:
1431:
1422:
1384:
1375:
1335:
1308:
1287:
1266:
1261:
1253:
1208:
1207:
1178:
1177:
1166:
1165:
1137:
1131:
1124:
1122:
1112:
1106:
1100:
1094:
1088:
1082:
1076:
1070:
1063:
1061:
1057:
1054:
1053:
991:
977:
962:
946:and inboard
933:
929:
925:drooped nose
910:
888:engine with
876:
859:
849:
840:
838:
829:landing gear
814:
803:
779:
757:West Germany
750:
739:
707:leading edge
689:
681:
667:
659:
637:
625:
623:
604:
597:
568:
549:
533:
520:
497:
483:
479:
477:
452:
433:
421:
419:
405:
401:
397:
393:
383:
353:
339:
316:
288:
264:Cardigan Bay
241:
225:to meet the
222:
214:
204:
192:
180:drooped nose
147:
143:
139:
137:
129:
125:
113:First flight
108:Experimental
92:Number built
82:Primary user
63:Manufacturer
18:
4327:Helicopters
4169:Heston JC.6
4114:Bristol 188
4050:/Sea Prince
4003:Avro Athena
3931:Avro Vulcan
3610:Helicopters
3396:Bolingbroke
3326:Beaufighter
3316:Blenheim IF
3276:F.2 Fighter
2350:Firefly IIM
2290:Hamble Baby
2150:Jet Provost
1195:Bristol 188
1156:Peter Twiss
1125:Performance
1113:Powerplant:
1000:RAF Cosford
971:RAF Cosford
913:cylindrical
894:air intakes
727:interceptor
664:yourself."
556:Rolls-Royce
430:Peter Twiss
344:Farnborough
274:. In 1947,
233:Development
188:Peter Twiss
4453:Categories
4214:Short SC.1
4209:Short SB.5
4204:Short SB.3
4184:Saro P.531
3998:Avro Anson
3575:Buckingham
3468:Buckingham
3451:Transports
3442:Buckmaster
3391:Bloodhound
3347:Ten-Seater
2480:Gannet AEW
2310:Flycatcher
2165:One-Eleven
1221:References
1095:Wing area:
906:air brakes
711:area ruled
618:See also:
584:RAF Sopley
572:Chichester
303:supersonic
299:Korean War
248:delta wing
238:Background
211:ogee delta
176:delta wing
172:supersonic
4254:Transport
4089:BAC TSR-2
3640:Designers
3627:Belvedere
3473:Freighter
3375:Britannia
3362:Type 142
3352:Taxiplane
3301:Bullfinch
3251:Scout A-D
2524:Tipsy S.2
2435:Spearfish
2425:Barracuda
2390:Swordfish
2355:Fleetwing
2340:Firefly I
2335:Kangourou
2320:Fremantle
2155:Lightning
1906:0143-5450
1226:Citations
1200:Avro 707C
1083:Wingspan:
1055:Data from
1007:Operators
986:Yeovilton
948:elevators
854:hydraulic
576:RNAS Ford
493:Hampshire
366:monoplane
348:SBAC Show
319:transonic
168:transonic
162:from the
128:), 1973 (
4418:EoN Eton
4084:Avro 707
4013:BAE Hawk
3990:Trainers
3791:fighters
3726:Fighters
3622:Type 173
3617:Sycamore
3589:Sporting
3570:Beaufort
3560:Blenheim
3550:Berkeley
3529:Type 221
3524:Type 188
3519:Type 138
3370:Brabazon
3321:Type 146
3311:Type 133
3306:Type 123
3244:Fighters
2568:aircraft
2492:aircraft
2475:Rotodyne
2440:Gyrodyne
2415:Albacore
2295:Campania
2257:aircraft
2203:Concorde
2191:programs
2106:aircraft
2050:Archived
1881:Bell X-1
1809:Archived
1145:See also
944:ailerons
917:fuselage
886:turbojet
879:tailless
782:Concorde
723:Red Dean
703:fairings
642:Ferranti
638:ER.103/C
626:ER.103/B
512:Bordeaux
438:flameout
361:and the
207:Concorde
4410:Gliders
4094:BAe EAP
3918:Bombers
3907:(naval)
3601:Brownie
3580:Brigand
3545:Braemar
3538:Bombers
3514:Type 92
3463:Brandon
3405:Trainer
3357:Pullman
3296:Bulldog
3291:Bagshot
3261:Scout F
3256:Scout E
3237:By role
2583:Boxkite
2566:Bristol
2519:Tipsy M
2509:Tipsy B
2465:Delta 2
2455:Delta 1
2395:Fantôme
2305:Pintail
2213:Tornado
2160:MUSTARD
2112:Numeric
1856:, p.137
1089:Height:
1077:Length:
921:tapered
850:BAC 221
776:BAC 221
644:-built
574:and at
524:nozzles
359:biplane
215:BAC 221
121:Retired
100:History
3848:Strike
3565:Bisley
3555:Bombay
3504:Bullet
3458:Bombay
3342:Tourer
3281:Badger
2603:Type T
2588:Glider
2576:scheme
2450:Gannet
2445:Primer
2420:Fulmar
2410:P.4/34
2405:Seafox
2400:Battle
2385:G.4/31
2375:S.9/30
2365:Gordon
2360:Hendon
2325:Ferret
2255:Fairey
2208:Jaguar
2028:
2013:
1998:
1983:
1952:
1937:
1918:
1904:
1852:
1828:Flight
1782:Flight
1770:Flight
1755:Flight
1732:Flight
1520:Flight
1138:Range:
1018:
904:-type
898:eyelid
890:reheat
865:Design
744:, the
731:strike
662:Mirage
536:reheat
464:Norway
460:France
387:Mach 1
178:and a
148:Type V
124:1966 (
74:Status
3789:Naval
3509:Racer
3427:P.B.8
3422:T.B.8
2633:P.B.8
2628:T.B.8
2623:B.R.7
2380:TSR.1
2180:TSR-2
2143:Names
1968:"The
1863:Notes
1071:Crew:
992:WG777
978:WG774
963:WG777
940:spars
902:petal
841:WG774
580:radar
484:WG777
480:WG777
434:WG774
422:WG774
406:WG774
402:WG777
398:WG777
394:WG774
340:WG774
324:swept
268:Wales
130:WG774
126:WG777
3596:Babe
3063:142M
3009:110A
2370:Seal
2315:Fawn
2285:N.10
2198:AFVG
2026:ISBN
2011:ISBN
1996:ISBN
1981:ISBN
1950:ISBN
1935:ISBN
1916:ISBN
1902:ISSN
1850:ISBN
1115:1 ×
846:PERT
786:ogee
780:The
733:and
648:and
590:and
410:flap
396:and
310:and
270:and
260:VTOL
170:and
138:The
46:Type
3499:X.3
3494:X.2
3228:223
3223:213
3218:200
3213:198
3208:193
3203:192
3198:191
3193:188
3188:182
3183:176
3178:175
3173:174
3168:173
3163:172
3158:171
3153:170
3148:167
3143:166
3138:165
3133:164
3128:163
3123:162
3118:161
3113:160
3108:159
3103:158
3098:156
3093:152
3088:149
3083:148
3078:146
3073:144
3068:143
3059:142
3054:138
3049:137
3044:135
3039:133
3034:130
3029:124
3024:123
3019:120
3014:118
3004:109
2999:107
2994:105
2989:101
2643:X.3
2638:X.2
2330:Fox
2300:III
2280:N.9
2275:N.4
2270:F.2
2134:221
2129:167
2124:166
2119:145
998:at
984:at
969:at
755:of
632:or
491:in
372:of
144:FD2
142:or
4455::
2984:99
2979:96
2974:95
2969:93
2964:92
2959:91
2954:90
2949:89
2944:88
2939:86
2934:84
2929:83
2924:81
2919:79
2914:77
2909:76
2904:75
2899:73
2894:72
2889:71
2884:62
2879:57
2874:55
2869:53
2864:52
2859:48
2854:47
2849:46
2844:45
2839:44
2834:43
2829:42
2824:37
2819:36
2814:33
2809:32
2804:31
2799:30
2794:29
2789:28
2784:27
2779:26
2774:25
2769:24
2764:23
2759:22
2754:21
2749:20
2744:18
2739:17
2734:16
2729:15
2724:14
2719:13
2714:12
2709:11
2704:10
1798:^
1762:^
1739:^
1654:^
1624:^
1584:^
1563:^
1536:^
1504:^
1483:^
1467:^
1449:^
1408:^
1396:^
1343:^
1317:^
1296:^
1275:^
1233:^
908:.
510:,
400:.
266:,
3706:e
3699:t
3692:v
3061:/
2700:9
2696:8
2691:7
2686:6
2681:5
2676:4
2671:3
2666:2
2661:1
2558:e
2551:t
2544:v
2247:e
2240:t
2233:v
2096:e
2089:t
2082:v
2063:.
2047:.
2032:.
2017:.
2002:.
1987:.
1956:.
1941:.
1883:.
1073:1
1002:.
988:.
209:"
132:)
95:2
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