Avro Vulcan

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Avro Vulcan
Avro Vulcan Bomber RAF.JPEG
A Vulcan B.2 of the RAF
RoleStrategic bomber
National originUnited Kingdom
ManufacturerA V Roe & Co (Avro)
Hawker Siddeley Aviation
DesignerRoy Chadwick/Stuart Davies
First flight30 August 1952
Introduction20 July 1956
RetiredMarch 1984
StatusRetired from service
Primary userRoyal Air Force
Number built136 (including prototypes)
Unit cost
£750,000 (1956)[1]
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Avro Vulcan
Avro Vulcan Bomber RAF.JPEG
A Vulcan B.2 of the RAF
RoleStrategic bomber
National originUnited Kingdom
ManufacturerA V Roe & Co (Avro)
Hawker Siddeley Aviation
DesignerRoy Chadwick/Stuart Davies
First flight30 August 1952
Introduction20 July 1956
RetiredMarch 1984
StatusRetired from service
Primary userRoyal Air Force
Number built136 (including prototypes)
Unit cost
£750,000 (1956)[1]

The Avro Vulcan (officially Hawker Siddeley Vulcan[2] from July 1963)[3] is a jet-powered delta wing strategic bomber, which was operated by the Royal Air Force (RAF) from 1956 until 1984. Aircraft manufacturer A.V. Roe and Company (Avro) designed the Vulcan in response to Specification B.35/46. Of the three V bombers produced, the Vulcan was considered the riskiest option. Several scale aircraft, designated Avro 707, were produced to test and refine the delta wing design principles.

The Vulcan B.1 was first delivered to the RAF in 1956; deliveries of the improved Vulcan B.2 started in 1960. The B.2 featured more powerful engines, a larger wing, an improved electrical system and electronic countermeasures (ECM); many were modified to accept the Blue Steel missile. As a part of the V-force, the Vulcan was the backbone of the United Kingdom’s airborne nuclear deterrent during much of the Cold War. Although the Vulcan was typically armed with nuclear weapons, it was capable of conventional bombing missions, a capability which was used in Operation Black Buck during the Falklands War between the United Kingdom and Argentina in 1982.

The Vulcan had no defensive weaponry, initially relying upon high-speed high-altitude flight to evade interception. Electronic countermeasures were employed by the B.1 (designated B.1A) and B.2 from circa 1960. A change to low-level tactics was made in the mid-1960s. In the mid-1970s nine Vulcans were adapted for maritime radar reconnaissance operations, redesignated as B.2 (MRR). In the final years of service six Vulcans were converted to the K.2 tanker configuration for aerial refuelling.

Since retirement by the RAF one example, B.2 XH558, named "The Spirit of Great Britain" has been restored for use in display flights and air shows, whilst two other B.2s, XL426 and XM655, are kept in taxiable condition for ground runs and demonstrations at London Southend Airport and Wellesbourne Mountford Airfield respectively.



Further information: V bombers
Silhouettes of an early Avro 698 concept and the cancelled Avro 710.

The origin of the Vulcan and the other V bombers is linked with early British atomic weapon programme and nuclear deterrent policies. Britain's atom bomb programme began with Air Staff Operational Requirement OR.1001 issued in August 1946. This anticipated a government decision in January 1947 to authorise research and development work on atomic weapons, the U.S. Atomic Energy Act of 1946 (McMahon Act) having prohibited exporting atomic knowledge, even to countries that had collaborated on the Manhattan Project.[4] OR.1001 envisaged a weapon not to exceed 24 ft 2 in (7.37 m) in length, 5 ft (1.5 m) in diameter and 10,000 lb (4,500 kg) in weight. The weapon had to be suitable for release from 20,000 ft (6,100 m) to 50,000 ft (15,000 m).[5]

In January 1947, the Ministry of Supply distributed Specification B.35/46 to UK aviation companies to satisfy Air Staff Operational Requirement OR.229 for "a medium range bomber landplane capable of carrying one 10,000 lb (4,500 kg) bomb to a target 1,500 nautical miles (1,700 mi; 2,800 km) from a base which may be anywhere in the world." A cruising speed of 500 knots (580 mph; 930 km/h) at heights between 35,000 ft (11,000 m) and 50,000 ft (15,000 m) was specified. The maximum weight when fully loaded ought not to exceed 100,000 lb (45,000 kg). In addition to a "Special" (i.e., atomic) bomb, the aircraft was to be capable of alternatively carrying a conventional bomb load of 20,000 lb (9,100 kg). The similar OR.230 required a "long range bomber" with a 2,000 nautical miles (2,300 mi; 3,700 km) radius of action with a maximum weight of 200,000 lb (91,000 kg) when fully loaded; this requirement was considered too difficult.[6] A total of six companies would submit technical brochures to this specification, including Avro.[7]

Required to tender by the end of April 1947, work began on receipt of Specification B.35/46 at Avro, led by technical director Roy Chadwick and chief designer Stuart Davies; the type designation was Avro 698. It was obvious to the design team that conventional aircraft could not satisfy the Specification; knowing little about high-speed flight and unable to glean much from the Royal Aircraft Establishment or the US, they investigated German Second World War swept wing research. The team estimated that an otherwise conventional aircraft, with a swept wing of 45°, would have doubled the weight requirement. Realising that swept wings increase longitudinal stability, the team deleted the tail (empennage) and the supporting fuselage, it thus became a swept-back flying wing with only a rudimentary forward fuselage and a fin (vertical stabilizer) at each wingtip. The estimated weight was now only 50% over the requirement; a delta shape resulted from reducing the wingspan and maintaining the wing area by filling in the space between the wingtips, which enabled the specification to be met.[8] Though Dr Alexander Lippisch is generally credited as the pioneer of the delta wing, Chadwick’s team had followed its own logical design process.[9] The initial design submission had four large turbojets stacked in pairs buried in the wing either side of the centreline. Outboard of the engines were two bomb-bays.[8]

In August 1947, Roy Chadwick was killed in the crash of the Avro Tudor 2 prototype and was succeeded by Sir William Farren.[10] Reductions in wing thickness made it impossible to incorporate the split bomb bays and stacked engines, thus the engines were placed side-by-side in pairs either side of a single bomb-bay, the fuselage growing somewhat. The wingtip fins gave way to a single fin on the aircraft's centreline.[8] Rival manufacturer Handley Page received a prototype contract for its crescent-winged HP.80 B.35/46 tender in November 1947.[10] Though considered the best option, contract placement for Avro's design was delayed whilst its technical strength was established.[11] Instructions to proceed with the construction of two Avro 698 prototypes was received in January 1948.[10] As an insurance measure against both radical designs failing, Short Brothers received a contract for the prototype SA.4 to the less-stringent Specification B.14/46; the SA.4, later named Sperrin, was not required. In April 1948, Vickers also received authority to proceed with their Type 660 which, although falling short of the B.35/46 Specification, being of a more conventional design would be available sooner; this plane entered service as the Valiant.[12]

Avro 707 and Avro 710[edit]

The prototype Vulcans (VX777 front, VX770 rear) with four Avro 707s at Farnborough in September 1953
Main article: Avro 707

As Avro had no flight experience of the delta wing, the company planned two smaller experimental aircraft based on the 698, the one-third scale model 707 for low-speed handling and the one-half scale model 710 for high-speed handling. Two of each were ordered. However, the 710 was cancelled when it was considered too time-consuming to develop; a high-speed variant of the 707 was designed in its place, the 707A.[13] The first 707, VX784, flew in September 1949 but crashed later that month killing the pilot, Avro test pilot Flt Lt Eric Esler. The second low-speed 707, VX790, built with the still uncompleted 707A’s nose section (containing an ejection seat)[14] and redesignated 707B, flew in September 1950 piloted by Avro test pilot Wg Cdr Roland "Roly" Falk. The high speed 707A, WD480, followed in July 1951.[15]

Due to the delay of the 707 programme, the contribution of the 707B and 707A towards the basic design of the 698 was not considered significant,[16] though it did highlight a need to increase the length of the nosewheel to give a ground incidence of 3.5 degrees, the optimum take-off attitude.[17] The 707B and 707A proved the design's validity and gave confidence in the delta planform. A second 707A, WZ736 and a two-seat 707C, WZ744 were also constructed but they played no part in the 698's development.[15]

Vulcan B.1 and B.2[edit]

Prototypes and type certification[edit]

More influential than the 707 in the 698's design was wind-tunnel testing performed by the Royal Aircraft Establishment at Farnborough, which indicated the need for a wing redesign to avoid the onset of compressibility drag which would have restricted the maximum speed.[18] Painted gloss white, the 698 prototype VX770 flew for the first time on 30 August 1952 piloted by Roly Falk flying solo. The prototype 698, then fitted with only the first-pilot's ejection seat and a conventional control wheel, was powered by four Rolls-Royce RA.3 Avon engines of 6,500 lbf (29 kN) thrust; there were no wing fuel tanks, temporary tankage was carried in the bomb bay.[19] VX770 made an appearance at the 1952 Society of British Aircraft Constructors' (SBAC) Farnborough Air Show the next month when Falk demonstrated an "almost vertical bank".[20] After its Farnborough appearance, the future name of the Avro 698 was a subject of speculation; Avro had strongly recommended the name Ottawa,[N 1] in honour of the company's connection with Avro Canada.[11][21] Weekly magazine Flight suggested Albion after rejecting Avenger, Apollo and Assegai. The Chief of the Air Staff preferred a V-class of bombers, the Air Council announced the following month that the 698 would be called Vulcan after the Roman god of fire and destruction.[22] In January 1953, VX770 was grounded for the installation of wing fuel tanks, Armstrong Siddeley ASSa.6 Sapphire engines of 7,500 lbf (33 kN) thrust and other systems; it flew again in July 1953.[23]

Comparison of Vulcan wing designs

The second prototype, VX777, flew in September 1953. More representative of production aircraft, it was lengthened to accommodate a longer nose undercarriage leg, featured a visual bomb-aiming blister under the cabin and was fitted with Bristol Olympus 100 engines of 9,750 lbf (43.4 kN) thrust. At Falk’s suggestion, a fighter-style control stick replaced the control wheel. Both prototypes had almost pure delta wings with straight leading edges. During trials in July 1954, VX777 was substantially damaged in a heavy landing at Farnborough. It was repaired and fitted with Olympus 101 engines of 11,000 lbf (49 kN) thrust before resuming trials in October 1955. While exploring the high speed and high altitude flight envelope, mild buffeting and other undesirable flight characteristics were experienced while approaching the speed of sound, including an alarming tendency to enter an uncontrollable dive, unacceptable to the Aeroplane and Armament Experimental Establishment (A&AEE) at Boscombe Down. The solution included the "Phase 2" wing, featuring a kinked and drooped leading edge and vortex generators on the upper surface, first tested on 707A WD480. An auto-mach trimmer introduced a nose-up attitude when at high speeds, the control column had to be pushed rather than pulled to maintain level flight.[24]

Meanwhile, the first production B.1,[N 2] XA889, had flown in February 1955 with the original wing.[26] In September 1955, Falk, flying the second production B.1 XA890 amazed crowds at the Farnborough Air Show by executing a barrel roll[27] on his second flypast in front of the SBAC president’s tent. After two days flying, he was called in front of service and civil aviation authorities and ordered to refrain from carrying out this "dangerous" manoeuvre.[27] Now fitted with a Phase 2 wing, XA889 was delivered in March 1956 to the A&AEE for trials for the type’s initial Certificate of Airworthiness which it received the following month.[28]

Further developments[edit]

The first 15 B.1s were powered by the Olympus 101 of 11,000 lbf (49 kN) thrust. Many of these early examples in a metallic finish remained the property of the Ministry of Supply being retained for trials and development purposes. Those entering RAF service were delivered to No 230 Operational Conversion Unit (OCU), the first in July 1956.[29] Later aircraft, painted in anti-flash white and powered by the Olympus 102 of 12,000 lbf (53 kN) thrust, began to enter squadron service in July 1957.[30] The Olympus 102s were quickly modified to Olympus 104 standard, ultimately rated at 13,500 lbf (60 kN) thrust.[31] As far back as 1952, Bristol Aero Engines had begun development of the BOl.6 (Olympus 6) rated at 16,000 lbf (71 kN) thrust[32] but if fitted to the B.1, this would have re-introduced the buffet requiring further redesign of the wing.[33]

The decision to proceed with the B.2 versions of the Vulcan was made in May 1956. It was anticipated that the first B.2 would be around the 45th aircraft of the 99 then on order.[34] As well as being able to achieve greater heights over targets, it was believed that operational flexibility could be extended by the provision of in-flight refuelling equipment and tanker aircraft.[35] The increasing sophistication of Soviet air defences required the fitting of electronic countermeasure (ECM) equipment and vulnerability could be reduced by the introduction of the Avro Blue Steel stand-off missile, then in development.[36] In order to develop these proposals, the second Vulcan prototype VX777 was rebuilt with the larger and thinner Phase 2C wing, improved flying control surfaces and Olympus 102 engines, first flying in this configuration in August 1957.[37] Plans were in hand to equip all Vulcans from the 16th aircraft onwards with in-flight refuelling receiving equipment.[38] A B.1, XA903, was allocated for Blue Steel development work. Other B.1s were used for the development of the BOl.6 (later Olympus 200), XA891; a new AC electrical system, XA893; and ECM including jammers within a bulged tail-cone and a tail-warning radar, XA895.[39]

The first Avro Vulcan B.2, XH533, flying at Farnborough, 1958.

The 46th production aircraft and first B.2, XH533, first flew in September 1958 fitted with Olympus 200 engines of 16,000 lbf (71 kN) thrust, six months before the last B.1 XH532 was delivered in March 1959.[40] Rebuilding B.1s as B.2s was considered but rejected over cost. Nevertheless, to extend the B.1's service life, 28 were upgraded by Armstrong Whitworth between 1959 and 1963 to the B.1A standard, including features of the B.2 such as ECM equipment,[41] in-flight refuelling receiving equipment,[42] and UHF radio.[43] The second B.2, XH534, flew in January 1959. Powered by production Olympus 201 of 17,000 lbf (76 kN) thrust, it was more representative of a production aircraft, being fitted with an in-flight refuelling probe and a bulged ECM tail cone. Some subsequent B.2s were initially lacking probes and ECM tail cones, but these were fitted retrospectively. The first 10 B.2s outwardly showed their B.1 ancestry, retaining narrow engine air intakes. Anticipating even more powerful engines, the air intakes were deepened on the 11th (XH557) and subsequent aircraft. Many of the early aircraft were retained for trials and it was the 12th B.2, XH558, that was the first to be delivered to the RAF in July 1960.[44]

The 26th B.2, XL317, the first of a production batch ordered in February 1956, was the first Vulcan, apart from development aircraft, capable of carrying the Blue Steel missile; 33 aircraft were delivered to the RAF with these modifications.[45] When the Mk.2 version of Blue Steel was cancelled in favour of the Douglas GAM-87 Skybolt air-launched ballistic missile in December 1959,[46] fittings were changed in anticipation of the new missile, one under each wing. Though Skybolt was cancelled in November 1962, many aircraft were delivered or retrofitted with "Skybolt" blisters.[47] Later aircraft (XL391 and XM574 onwards) were delivered with Olympus 301 engines of 20,000 lbf (89 kN) thrust. Two earlier aircraft were re-engined (XH557 and XJ784) for trials and development work; another seven aircraft (XL384-XL390) were converted circa 1963.[48]

The last B.2 was delivered in 1965 and the type served till 1984. Whilst in service the B.2 was continuously updated with modifications including rapid engine starting, bomb-bay fuel tanks, wing strengthening to give the fatigue life to enable the aircraft to fly at low level (a tactic introduced in the mid-60s), upgraded navigation equipment, Terrain Following Radar (TFR), standardisation on a common nuclear weapon (WE.117) and improved ECM equipment.[49] The B.1As were not strengthened, thus all were withdrawn by 1968.[50] Nine B.2s were modified for the Maritime Radar Reconnaissance (MRR) role[51] and six for the airborne tanker role.[52]

Proposed developments and cancelled projects[edit]

Avro Type 718

The Avro 718 was a 1951 proposal for a delta-winged military transport based on the Type 698 to carry 80 troops or 110 passengers. It would have been powered by four Bristol Olympus BOl.3 engines.[53]

Avro Atlantic
Main article: Avro Atlantic

The Avro Type 722 Atlantic was a 1952 proposal (announced in June 1953) for a 120-passenger delta-winged airliner based on the Type 698.[53]

Avro Type 732

The Avro 732 was a 1956 proposal for a supersonic development of the Vulcan and would have been powered by 8 de Havilland Gyron Junior engines. Unlike the proposed Avro 721 low-level bomber of 1952 or the Avro 730 supersonic stainless steel canard bomber dating from 1954 (cancelled in 1957 before completion of the prototype), the Type 732 showed its Vulcan heritage.[53]

Vulcan Phase 6 (Vulcan B.3)
Silhouette of the original study for the Vulcan B.3 Patrol Missile Carrier.

In 1960, the Air Staff approached Avro with a request into a study for a Patrol Missile Carrier armed with up to six Skybolt missiles capable of a mission length of 12 hours. Avro's submission in May 1960 was the Phase 6 Vulcan, which if built would have been the Vulcan B.3. The aircraft was fitted with an enlarged wing of 121 ft (37 m) span with increased fuel capacity; additional fuel tanks in a dorsal spine; a new main undercarriage to carry an all-up-weight of 339,000 lb (154,000 kg); and reheated Olympus 301s of 30,000 lbf (130 kN) thrust. An amended proposal of October 1960 inserted a 10 ft 9 in (3.28 m) plug into the forward fuselage with capacity for six crew members including a relief pilot, all facing forwards on ejection seats, and aft-fan versions of the Olympus 301.[54]

Export proposals[edit]

Other countries expressed interest in purchasing Vulcans but, as with the other V-bombers, no foreign sales materialised.[55]


As early as 1954, Australia recognised that the English Electric Canberra was becoming outdated and evaluated aircraft such as the Avro Vulcan and Handley-Page Victor as potential replacements.[56] Political pressure for a Canberra replacement only rose to a head in 1962; at which point more modern types such as the BAC TSR-2, General Dynamics F-111C, and North American A-5 Vigilante had become available. The RAF would have transferred several V-bombers, including Vulcans, for interim use by the RAAF if they had purchased the TSR-2, but the RAAF selected the F-111C.[57][58][59]


In the early 1980s, Argentina approached the UK with a proposal to buy a number of Vulcans. An application, made in September 1981, requested the 'early availability' of a 'suitable aircraft'. With some reluctance, ministers approved the export of a single aircraft but emphasised that clearance had not been given for the sale of a larger number. A letter from the British Foreign and Commonwealth Office to the Ministry of Defence in January 1982 stated that little prospect was seen of this happening without ascertaining the Argentine interest and whether such interest was genuine: 'On the face of it, a strike aircraft would be entirely suitable for an attack on the Falklands.'[60] Argentina invaded the Falkland Islands less than three months later.


Avro Vulcan XH558 at Duxford Airshow 2012


In spite of its radical and unusual shape, the airframe was built along traditional lines. Except for the most highly stressed parts, the whole structure was manufactured from standard grades of light alloy. The airframe was broken down into a number of major assemblies: the centre section, a rectangular box containing the bomb-bay and engine bays bounded by the front and rear spars and the wing transport joints; the intakes and centre fuselage; the front fuselage, incorporating the pressure cabin; the nose; the outer wings; the leading edges; the wing trailing edge and tail end of the fuselage; the wings were not sealed and used directly as fuel tankage, but carried bladders for fuel in the void spaces of the wings; and there was a single swept tail fin with a single rudder on the trailing edge.[61]

A five-man crew, the first pilot, co-pilot, navigator radar, navigator plotter and air electronics officer (AEO) was accommodated within the pressure cabin on two levels; the pilots sitting on Martin-Baker 3K (3KS on the B.2) ejection seats whilst on the lower level, the other crew sat facing rearwards and would abandon the aircraft via the entrance door.[62][63] The original B35/46 specification sought a jettisonable crew compartment, this requirement was removed in a subsequent amendment, the rear crew's escape system was often an issue of controversy, such as when a practical refit scheme was rejected.[64][65] A rudimentary sixth seat forward of the navigator radar was provided for an additional crew member;[66] the B.2 had an additional seventh seat opposite the sixth seat and forward of the AEO. These seats were no more than cushions, a full harness and an oxygen and intercom facility. The visual bomb-aimer’s compartment could be fitted with a T4 (Blue Devil) bombsight,[67] in many B.2s this space housed a vertically mounted Vinten F95 Mk.10 camera for assessing simulated low-level bombing runs.[68]

Fuel was carried in 14 bag tanks, four in the centre fuselage above and to the rear of the nosewheel bay and five in each outer wing. The tanks were split into four groups of almost equal capacity, each normally feeding its respective engine though cross-feeding was possible. The centre of gravity was automatically maintained by electric timers which sequenced the booster pumps on the tanks.[62][69] B.2 aircraft could be fitted with one or two additional fuel tanks in the bomb-bay.[70]

Despite being designed before a low radar cross-section (RCS) and other stealth factors were ever a consideration,[71] a Royal Aircraft Establishment technical note of 1957 stated that of all the aircraft so far studied, the Vulcan due to its shape appeared by far the simplest radar echoing object: only one or two components contributing significantly to the echo at any aspect, compared with three or more on most other types.[72][N 3]


The original Vulcan B.1 radio fit was: two 10-channel VHF transmitter/receivers (TR-1985/TR-1986) and a 24-channel HF transmitter/receiver (STR-18).[77] The Vulcan B.1A also featured an UHF transmitter/receiver (ARC-52).[43] The initial B.2 radio fit was similar to the B.1A[78] though it was ultimately fitted with the ARC-52, a V/UHF transmitter/receiver (PTR-175), and a SSB HF transmitter/receiver (Collins 618T).[79]

The Navigation and Bombing System (NBS) comprised an H2S Mk9 radar and a Navigation Bombing Computer (NBC) Mk1.[77] Other B.1 navigation aids included a Marconi radio compass (ADF), GEE Mk3, Green Satin Doppler radar to determine the groundspeed and drift angle, radio and radar altimeters, and ILS.[77] TACAN replaced GEE in the B.1A[80] and B.2 and Decca Doppler 72 replaced Green Satin in the B.2.[81] A continuous display of the aircraft's position was maintained by a Ground Position Indicator (GPI).[81]

Vulcan B.2s were eventually fitted with the twin-gyro free-running gyroscopic Heading Reference System (HRS) Mk.2, based upon the inertial platform of the Blue Steel missile, which had been integrated into the system when the missile had been carried.[81] With the HRS a Navigator's Heading Unit (NHU)was provided which enabled the Navigator Plotter to adjust the aircraft heading, through the autopilot, by as little as 0.1 degrees. The B.2 (MRR) was additionally fitted with the LORAN C navigation system.[51]

The original ECM fit as fitted to the B.1A and B.2 was: one Green Palm voice communications' jammer; two Blue Diver metric jammers; three Red Shrimp S-band jammers; ; a Blue Saga Passive Warning Receiver with 4 aerials (PWR); one Red Steer tail-warning radar; and window (chaff) dispensers.[82] The bulk of the equipment was carried in a large extended tail cone, and a flat ECM aerial counterpoise plate mounted between the starboard tailpipes.[83][N 4] Later equipment on the B.2 included: an L-band jammer (replacing a Red Shrimp); the ARI 18146 X-band jammer;[85] replacing the Green Palm; the improved Red Steer Mk.2; infra-red decoys (flares); and the ARI 18228 PWR with its aerials that gave a squared top to the fin.[78][86]

Colour schemes[edit]

Aerial view of a Vulcan B.2 in late RAF markings on static display at RAF Mildenhall

The two prototype Vulcans were finished in gloss white. Early Vulcan B.1s left the factory in a natural metal finish; the front half of the nose radome was painted black, the rear half painted silver. Front-line Vulcan B.1s had a finish of anti-flash white and RAF "type D" roundels. Front-line Vulcan B.1As and B.2s were similar but with 'type D pale' roundels.[87]

With the adoption of low-level attack profiles in the mid-1960s, B.1As and B.2s were given a glossy Sea Grey Medium and Dark Green disruptive pattern camouflage on the upper surfaces, white undersurfaces and "type D" roundels. (The last 13 Vulcan B.2s, XM645 onwards, were delivered thus from the factory[88]). In the mid-1970s: Vulcan B.2s received a similar scheme with matte camouflage, Light Aircraft Grey undersides, and "low-visibility" roundels; B.2(MRR)s received a similar scheme in gloss; and the front half of the radomes were no longer painted black. Beginning in 1979, 10 Vulcans received a wrap-around camouflage of Dark Sea Grey and Dark Green[89][90] because, during Red Flag exercises in the USA, defending SAM forces had found that the grey-painted undersides of the Vulcan became much more visible against the ground at high angles of bank.[91]


Vulcan B.1 XA890 in early silver scheme landing at Farnborough in September 1955 after Roly Falk's "aerobatic" display. Note the lower outer starboard airbrake, which was later deleted

The aircraft was controlled by a fighter-type control stick and rudder bar which operated the powered flying controls (PFCs). Each PFC had a single electro-hydraulic powered flying control unit (PFCU) except the rudder which had two, one running as a back-up. Artificial feel and autostabilisation in the form of pitch and yaw dampers were provided, as well as an auto mach trimmer.[92]

The flight instruments in the B.1 were traditional and included G4B compasses;[93] Mk.4 artificial horizons;[94] and zero reader flight display instruments.[95] The B.1 had a Smiths Mk10 autopilot.[96] In the B.2, these features were incorporated into the Smiths Military Flight System (MFS), the pilots' components being: two beam compasses; two director-horizons; and a Mk.10A or Mk.10B autopilot.[97] From 1966, B.2s were fitted with the ARI 5959 Terrain-following radar (TFR), built by General Dynamics,[98] its commands being fed into the director-horizons.[99]

The B.1 had four elevators (inboard) and four ailerons (outboard).[100] In the B.2, these were replaced by eight elevons.[101] The Vulcan was also fitted with six electrically-operated three-position (in, medium drag, high drag) airbrakes, four in the upper centre section and two in the lower.[102] There were originally four lower airbrakes but the outboard two were deleted before the aircraft entered service.[103] A brake parachute was installed inside the tail cone.[104]

Electrical and hydraulic systems[edit]

The main electrical system on the B.1/B.1A was 112V DC supplied by four 22.5kW engine-driven generators. Backup power was provided by four 24V 40Ah batteries connected in series providing 96V. Secondary electrical systems were 28V DC, single-phase 115V AC at 1600Hz, and three-phase 115V AC at 400 Hz, driven by transformers and inverters from the main system. The 28V DC system was backed up by a single 24V battery.[105]

For greater efficiency and higher reliability,[106] the main system on the B.2 was changed to three-phase 200V AC at 400 Hz supplied by four 40kVA engine-driven constant speed alternators. Standby supplies in the event of a main AC failure were provided by a Ram Air Turbine (RAT) driving a 17kVA alternator that could operate at high altitude down to 20,000 ft (6,100 m), and an Airborne Auxiliary Power Plant (AAPP),[107] a Rover[33] gas turbine driving a 40kVA alternator, which could be started once the aircraft was below an altitude of 30,000 ft (9,100 m). Secondary electrical supplies were similar to the B.1.[107]

The change to an AC system was a significant improvement. The Vulcan's powered flying controls were hydraulically actuated but each Powered Flying Control Unit (PFCU) had a hydraulic pump which was driven by an electrical motor.[108] Because there was no manual reversion, a total electrical failure would result in a loss of control. The standby batteries on the B.1 were designed to give enough power for 20 minutes of flying time but this proved to be optimistic and two aircraft, XA891 and XA908, crashed as a result.[109]

The main hydraulic system provided pressure for: undercarriage raising and lowering and bogie trim; nosewheel centring and steering; wheelbrakes (fitted with Maxarets); bomb doors opening and closing; and (B.2 only) AAPP air scoop lowering. Hydraulic pressure was provided by three hydraulic pumps fitted to Nos. 1, 2 and 3 engines. An electrically operated hydraulic power pack (EHPP) could be used to operate the bomb doors and recharge the brake accumulators. A compressed air (later nitrogen) system was provided for emergency undercarriage lowering.[110]


Main article: Rolls-Royce Olympus

The Rolls-Royce Olympus, originally known as the "Bristol BE.10 Olympus",[111][N 5] is a two-spool axial-flow turbojet that powered the Vulcan. Each Vulcan had four engines buried in the wings, positioned in pairs close to the centre of the fuselage. The engine's design began in 1947, intended to power the Bristol Aeroplane Company's own rival design to the Vulcan.[113] A serendipitous arrangement in air intakes can cause the Vulcan to emit a distinctive "howl" when the engines are at approximately 90% power,[114] which can be heard as the aircraft performs a flypast, such as at public airshows.[115][116]

Gas-flow diagram of an Olympus Mk 101 engine

As the prototype Vulcan VX770 was ready for flight prior to the Olympus being available, it first flew using Rolls-Royce Avon RA.3 engines of 6,500 lbf (29 kN) thrust. These were quickly replaced by Armstrong Siddeley Sapphire ASSa.6 engines of 7,500 lbf (33 kN) thrust.[117] VX770 later became a flying test bed for the Rolls-Royce Conway.[118] The second prototype VX777 first flew with Olympus 100s of 10,000 lbf (44 kN) thrust. It was subsequently re-engined with Olympus 101 engines of 11,000 lbf (49 kN) thrust.[119] When VX777 flew with a Phase 2C (B.2) wing in 1957, it was fitted with Olympus 102 engines of 12,000 lbf (53 kN) thrust.[120]

Early B.1s were engined with the Olympus 101. Later aircraft were delivered with Olympus 102s. All Olympus 102s became the Olympus 104 of 13,000 lbf (58 kN) thrust on overhaul and ultimately 13,500 lbf (60 kN) thrust on uprating.[121] The first B.2 flew with the second-generation Olympus 200 of 16,000 lbf (71 kN) thrust,[122] design of which began in 1952.[123] Subsequent B.2s were engined with either the uprated Olympus 201 of 17,000 lbf (76 kN) thrust or the Olympus 301 of 20,000 lbf (89 kN) thrust. The Olympus 201 was designated 202 on being fitted with a rapid air starter.[124] The engine would later be developed into a reheated (afterburning) powerplant for the cancelled supersonic BAC TSR-2 strike bomber and the supersonic passenger transport Concorde.[91]

Operational history[edit]


In September 1956, the RAF received its first Vulcan B.1, XA897, which immediately embarked upon a round-the-world tour. The tour was to be an important demonstration of the range and capabilities of the aircraft, it also had other benefits in the form of conducting goodwill visits in various countries; in later life Vulcans routinely visited various nations and distant parts of the former British Empire as a show of support and military protection.[125] This first tour, however, was struck by misfortune; on 1 October 1956, while landing in bad weather at London Heathrow Airport at the completion of the world tour, XA897 was destroyed in a fatal accident.[126]

A Vulcan B1A of the Waddington Wing at Filton during a public air display in the 1960s

The first two aircraft were delivered to 230 OCU in January 1957 and the training of crews started on 21 February 1957, in the following months more aircraft were delivered to the OCU.[109] The first OCU course to qualify was No. 1 Course, on 21 May 1957, and they went on to form the first flight of No.83 Squadron.[109] No. 83 Squadron was the first operational squadron to use the bomber, at first using borrowed Vulcans from the OCU and on 11 July 1956 it received the first aircraft of its own.[109] By September 1957, several Vulcans had been handed over to No.83 Squadron[127] The second OCU course also formed a Flight of 83 Squadron, but subsequent trained crews were also used to form the second bomber squadron, 101 Squadron.[109] The last aircraft from the first batch of 25 aircraft had been delivered by the end of 1957 to 101 Squadron.[109]

In order to increase the mission range and flight time for Vulcan operations, in-flight refuelling capabilities were added in 1959 onwards; several Valiant bombers were refurbished as tankers to refuel the Vulcans.[128] Continuous airborne patrols proved untenable, however, and the refuelling mechanisms across the Vulcan fleet fell into disuse in the 1960s.[128] Both Vulcans and the other V-force aircraft routinely visited the Far East, in particular Singapore, where a fully equipped nuclear weapons storage facility had been constructed in 1959.[129] During the Indonesia–Malaysia confrontation Britain planned to deploy three squadrons of V-bomber aircraft and 48 Red Beard tactical nuclear weapons to the region, although this was ultimately decided against, Vulcans trained in the region for both conventional and nuclear missions.[129] Britain regularly deployed of Vulcans to the Far East as a part of their contribution to SEATO operations, often to test the defenses of friendly nations in joint exercises.[129] In the early 1970s, the RAF decided to permanently deploy two squadrons of Vulcans overseas in the Near East Air Force Bomber Wing, based at RAF Akrotiri in Cyprus; the Vulcans were withdrawn as Cypriot intercommunal violence intensified in the mid-1970s.[130]

Royal Air Force Vulcan B.2 being prepared for flight on 25 May 1985

Vulcans did some very long range missions. In June 1961, one of them took off from RAF Scampton to Sydney, with an 18,507 km long journey, flown in only a bit more than 20 hours and three air refuellings. Vulcans frequently visited the United States during the 1960s and 1970s to participate in air shows and static displays, as well as to participate in the Strategic Air Command's Annual Bombing and Navigation Competition at such locations as Barksdale AFB, Louisiana and the former McCoy AFB, Florida, with the RAF crews representing Bomber Command and later Strike Command. Vulcans also took part in the 1960, 1961, and 1962 Operation Skyshield exercises, in which NORAD defences were tested against possible Soviet air attack, the Vulcans simulating Soviet fighter/bomber attacks against New York, Chicago and Washington. The results of the tests were classified until 1997.[131] The Vulcan proved quite successful during the 1974 'Giant Voice' exercise, in which it had managed to avoid USAF interceptors [132]

Nuclear deterrent[edit]

As part of Britain's independent nuclear deterrent, the Vulcan initially carried Britain's first nuclear weapon, the Blue Danube gravity bomb.[133] Blue Danube was a low-kiloton yield fission bomb designed before the United States detonated the first hydrogen bomb. These were supplemented by U.S.-owned Mk 5 bombs (made available under the Project E programme) and later by the British Red Beard tactical nuclear weapon.[134] The UK had previously embarked on its own hydrogen bomb programme, and to bridge the gap until these were ready the V-bombers were equipped with an Interim Megaton Weapon based on the Blue Danube casing containing Green Grass, a large pure-fission warhead of 400 kt (1.7 PJ) yield.[135][N 6] This bomb was known as Violet Club.[135] Only five were deployed before the Green Grass warhead was incorporated into a developed weapon as Yellow Sun Mk.1.[135]

The later Yellow Sun Mk 2, was fitted with Red Snow,[135] a British-built variant of the U.S. W28 warhead. Yellow Sun Mk 2 was the first British thermonuclear weapon to be deployed, and was carried on both the Vulcan and Handley Page Victor. The Valiant retained U.S. nuclear weapons assigned to SACEUR under the dual-key arrangements. Red Beard was pre-positioned in Singapore for use by Vulcan and Victor bombers.[138] From 1962, three squadrons of Vulcan B.2s and two squadrons of Victor B.2s were armed with the Blue Steel missile, a rocket-powered stand-off bomb, which was also armed with the 1.1 Mt (4.6 PJ) yield Red Snow warhead.[139]

Operationally, RAF Bomber Command and the U.S. Strategic Air Command cooperated in the Single Integrated Operational Plan (SIOP) to ensure coverage of all major Soviet targets from 1958, 108 aircraft of the RAF's V-Bombers were assigned targets under SIOP by the end of 1959.[140] From 1962 onwards, two jets in every major RAF base were armed with nuclear weapons and on standby permanently under the principle of Quick Reaction Alert (QRA).[140] Vulcans on QRA standby were to be airborne within four minutes of receiving an alert, as this was identified as the amount of time between warning of a USSR nuclear strike being launched and it arriving in Britain.[141] The closest the Vulcan came to take part in potential nuclear conflict was during the Cuban missile crisis in October 1962, where Bomber Command was moved to Alert Condition 3, an increased state of preparedness from normal operations, however stood down in early November.[142]

XH558 taking off; 2008 Farnborough Airshow

The Vulcans were intended to be equipped with the American Skybolt Air Launched Ballistic Missile to replace the Blue Steel, with Vulcan B.2s carrying two Skybolts under the wings; the last 28 B.2s were modified on the production line to fit pylons to carry the Skybolt.[143][144] A B.3 variant with increased wingspan to carry up to six Skybolts was proposed in 1960.[145] When the Skybolt missile system was cancelled by U.S. President John F. Kennedy on the recommendation of his Secretary of Defense, Robert McNamara in 1962, Blue Steel was retained. To supplement it until the Royal Navy took on the deterrent role with Polaris ICBM-equipped submarines, the Vulcan bombers adopted a new mission profile of flying high during clear transit, dropping down low to avoid enemy defences on approach, and deploying a parachute-retarded bomb, the WE.177B.[146] However, since the aircraft had been designed for high-altitude flight, at low altitudes it could not exceed 350 knots. RAF Air Vice Marshal Ron Dick, a former Vulcan pilot, said "it is [thus] questionable whether it could have been effective flying at low level in a war against ... the Soviet Union.”[147]

After the British Polaris submarines became operational and Blue Steel was taken out of service in 1970, the Vulcan continued to carry WE.177B in a tactical nuclear strike role as part of the British contribution to Europe's standing NATO forces, although they no longer held aircraft at 15 minutes readiness in peacetime.[146] Two squadrons were also stationed in Cyprus as part of the Near East Air Force and assigned to Central Treaty Organization in a strategic strike role. With the eventual demise of the WE.177B and the Vulcan bombers, the Blackburn Buccaneer, SEPECAT Jaguar, and Panavia Tornado, continued with the WE.177C until its retirement in 1998.[148] While not a like-for-like replacement, the multi-role Tornado interdictor/strike bomber is the successor for the roles previously filled by the Vulcan.[149]

Conventional role[edit]

A Vulcan at the National Museum of Flight, note the Operation Black Buck markings and internment in Brazil

Although in operational usage, the Vulcan typically carried various nuclear armaments, the type also had a conventional secondary role. While performing conventional combat missions, the Vulcan can carry up to 21 1,000 lb (454 kg) bombs inside its bomb bay.[150] Since the 1960s, the various Vulcan squadrons were routinely conducting conventional training missions; the aircrews were expected to be able to perform conventional bombing missions in addition to the critical nuclear strike mission the Vulcan normally performed.[151]

The only combat missions in which the Vulcan would conduct actually took place towards the end of the type's service in 1982. During the Falklands War, the Vulcan was deployed against Argentinian forces which had occupied the Falkland Islands. This conflict was the only occasion in which any of the V-bombers would participate in conventional warfare.[152] The missions performed by the Vulcan became known as the Black Buck raids, each aircraft had to fly 3,889 mi (6,259 km) from Ascension Island to reach Stanley on the Falklands. Victor tankers conducted the necessary air-to-air refuelling for the Vulcan to cover the distance involved; approximately 1.1 million gal (5 million L) of fuel were used in each mission.[153]

A total of five Vulcans had been selected to participate in the operation. In order to do so, each aircraft had to receive various last-minute adaptions; including modifications to the bomb bay, the reinstatement of the long out-of-use in-flight refuelling system, the installation of a new navigational system derived from the Vickers VC-10, the updating of several onboard electronics. Underneath the wings, new pylons were fitted to carry an ECM pod and Shrike anti-radar missiles at wing hardpoint locations; these hardpoints had originally been installed for the purpose of carrying the cancelled Skybolt nuclear missile. Engineering work to retrofit these Vulcans had begun on 9 April.[154][155]

A Vulcan flying over Ascension Island on 18 May 1982

On 1 May, the first mission was conducted by a single Vulcan that flew over Port Stanley and dropped its bombs on the airfield concentrating on the single runway, with one direct hit, making it unsuitable for fighter aircraft. The Vulcan's mission was quickly followed up by strikes against anti-air installations, flown by British Aerospace Sea Harriers from nearby Royal Navy carriers.[156] A total of three Vulcan missions were flown against the airfield, a further two missions in which missiles were launched against radar installations; an additional two missions were cancelled.[153] At the time, these missions held the record for the world's longest-distance raids.[150][157] The ECM systems on board the Vulcans proved to be effective at jamming Argentine radars; while a Vulcan was within the theatre, other British aircraft in the vicinity had a greatly reduced chance of coming under effective fire.[158][159]

On 3 June 1982, Vulcan B.2 XM597 of No. 50 Squadron took part in the "Black Buck 6" mission against Argentinian radar sites at Stanley airfield on the Falkland Islands. While attempting to refuel for its return journey to Ascension Island, the probe broke, leaving the Vulcan with insufficient fuel, forcing a diversion to Galeão Air Force Base, Rio de Janeiro in neutral Brazil. En route, secret papers were dumped along with the two remaining AGM-45 Shrike missiles, although one failed to launch. After a mayday call, the Vulcan, escorted by Brazilian Air Force Northrop F-5 fighters, was permitted an emergency landing at Rio with very little fuel left on board.[160] The Vulcan and her crew were detained until the end of hostilities nine days later.[161]

Maritime radar reconnaissance[edit]

In November 1973, No. 27 Squadron reformed at RAF Scampton in the maritime radar reconnaissance role. Though initially equipped with a number of B.2 aircraft,[162] the Squadron eventually operated nine B.2 (MRR) aircraft.[51] The main external visual difference was the presence of a gloss paint finish, with a light grey undersurface, to protect against sea spray. TFR was not fitted and the aircraft were equipped with LORAN C navigational equipment.[51] Five aircraft were further modified for the Squadron's secondary role of air sampling.[51] These aircraft were distinguishable by the additional hardpoints outside of the underwing Skybolt points upon which could be hung pylons and the air-sampling pods,[163] which had been constructed from de Havilland Sea Vixen drop tanks.[51]

Aerial refuelling role[edit]

After the end of the Falklands War in 1982, the Vulcan B.2 was due to be withdrawn from RAF service that year.[152] However, the Falklands campaign had consumed much of the airframe fatigue life of the RAF's Victor tankers. While Vickers VC10 tanker conversions had been ordered in 1979[164] and Lockheed TriStar tankers would be ordered subsequent to the conflict,[165] as a stopgap measure six Vulcans were converted into single point tankers. The Vulcan tanker conversion was accomplished by removing the jammers from the ECM bay in the tail of the aircraft, and replacing them with a single Hose Drum Unit (HDU).[155] An additional cylindrical bomb-bay tank was fitted, making a total of three, giving a fuel capacity of almost 100,000 lb (45,000 kg).[155][166]

The go-ahead for converting the six aircraft was given on 4 May 1982.[167] Just 50 days after being ordered, the first Vulcan tanker, XH561, was delivered to RAF Waddington.[155][167] The Vulcan K.2s were operated by No. 50 Squadron, along with three Vulcan B.2s, in support of UK air defence activities until it was disbanded in March 1984.[168]

Engine test beds[edit]


The initial production aircraft. First few with straight leading edge, later retrofitted with Phase 2 (kinked) wing. Early examples finished in silver, later changed to "anti-flash" white. Many converted to B.1A standard 1959-1963. Last few unmodified B.1s in RAF service with No. 230 OCU retired by 1966.[177] Last flight by any B.1, an engine testbed XA903, March 1979.[178]
The B.1 with an Electronic Countermeasures (ECM) system in a new larger tail cone (as in B.2).[179] Unlike the B.2, the B.1As did not undergo extensive wing strengthening for low-level flying[140][180] and were withdrawn from service 1966-67.[181]
Developed version of the B.1. Larger, thinner wing than the B.1 (Phase 2C wing) and fitted with Olympus 201-202 engines of 17,000 lbf (76 kN) each, or Olympus 301 engines of 20,000 lbf (89 kN) each. Uprated electrics with Auxiliary Airborne Power Plant (AAPP) (Auxiliary power unit) and Ram Air Turbine (RAT).[182] ECM similar to B.1A. Terrain-Following Radar (TFR) in nose thimble radome fitted to most aircraft in mid-60s. New Radar warning receiver aerials on tail fin giving it a square top from mid-1970s.[N 7]
B.2 (MRR)
Nine B.2s converted to Maritime Radar Reconnaissance (MRR). TFR deleted. Five aircraft further modified for Air Sampling Role. Distinctive gloss finish with light grey underside.[51]
Six B.2s converted for air-to-air refuelling with Mark 17 Hose Drum Unit (HDU) mounted semi-recessed in tail cone. TFR deleted. Fitted with three bomb-bay drum tanks, it was the only mark of Vulcan that could jettison fuel in an emergency.[186]
Proposed version intended as a long endurance missile carrier capable of carrying up to six Skybolt ALBMs on flights of up to 12 hours duration. Never built.[54]
Length97 feet 1 inch (29.59 m)105 feet 11 inches (32.28 m)110 feet 0 inches (33.53 m)
Height26 feet 6 inches (8.08 m)27 feet 2 inches (8.28 m)
Wingspan99 feet 0 inches (30.18 m)111 feet 0 inches (33.83 m)121 feet 0 inches (36.88 m)
Engines4 x Bristol-Siddeley Olympus 101/102/1044 x Bristol-Siddeley Olympus 201 or 3014 x Bristol-Siddeley Olympus 301
Armament1 x Blue Danube or Yellow Sun;
21 x 1000 lb free-fall bombs
1 x Blue Steel;
21 x 1000 lb free-fall bombs
Up to 6 x Skybolt


A total of 134 production Vulcans were assembled at Woodford Aerodrome, 45 to the B.1 design and 89 were B.2 models, the last being delivered to the RAF in January 1965.[182]

Contract DateQuantityVariantNotes
6 July 19482PrototypesTwo prototypes delivered in August 1952 and September 1953[187]
14 August 195225Vulcan B.1First flight of production aircraft 4 February 1955, delivered between June 1955 and December 1957.[187][188]
30 September 195420Vulcan B.1Delivered between January 1958 and April 1959.[187][189]
30 September 195417Vulcan B.2Delivered between September 1959 and December 1960[187][189]
31 March 19558Vulcan B.2Delivered between January and May 1961[187][190]
25 February 195624Vulcan B.2Delivered between July 1961 and November 1962[187][191]
22 January 195840Vulcan B.2Delivered between February 1963 and January 1965, one aircraft not flown and used as a static test airframe[187][192]


The Vulcan to the Sky Trust's Avro Vulcan XH558
 United Kingdom


Avro Vulcans of No 617 Squadron at RAF Cottesmore circa 1975.

V-Bomber dispersal airfields[edit]

In the event of transition to war, the V Bomber squadrons were to deploy four aircraft at short notice to each of 26 pre-prepared dispersal airfields around the United Kingdom. In the early 1960s the RAF ordered 20 Beagle Basset communication aircraft to move the crews to dispersal airfields; the importance of these aircraft was only brief, diminishing when the primary nuclear deterrent switched to the Royal Navy's Polaris Missile.[204]

Accidents and incidents[edit]

External images
Vulcan B.1 XA897
Vulcan B.1 XA897 prior to the accident, stopping over at RAF Khormaksar
The prototype Vulcan VX770 in 1954, retaining the original "pure delta" wing shape

Aircraft on display[edit]

Media related to Avro Vulcan museum aircraft at Wikimedia Commons

Avro Vulcan XL361 on display at CFB Goose Bay in 1988
Avro Vulcan XL319 on display at North East Aircraft Museum
XH558 performs its first post-restoration public display on 5 July 2008


Main article: Avro Vulcan XH558

The last airworthy Vulcan (XH558) has been restored to flying condition by the "Vulcan to the Sky Trust" after years of effort and fundraising. The first post-restoration flight, which lasted 34 minutes, took place on 18 October 2007.[203][247]

The aircraft's airworthiness status was in peril as maintenance funding was in need before the end of February 2010. At the last moment an anonymous benefactor presented £458,000 to the foundation, ensuring its airworthiness for both its 50th birthday and the prospect of a flight performance for the 2012 Summer Olympic Games opening ceremony in London.[248] It is currently based at Doncaster/Sheffield Robin Hood Airport, formerly RAF Finningley.[249]


Vulcan B.1[edit]

External images
Avro Vulcan B.2 cutaway showing internal compartments and bays
Avro Vulcan Cutaway from Flightglobal.com
Avro Vulcan B Mk 2.svg

Data from Polmar,[250] Laming[251]

General characteristics



Comparison of variants[edit]

Variants compared[252][253]
B.1B.1AB.2B.2 (MRR)K.2
Wingspan99 ft 5 in (30.30 m)111 ft 0 in (33.83 m)
Length97 ft 1 in (29.59 m)105 ft 6 in (32.16 m) [99 ft 11 in (30.45 m) without probe]
Height26 ft 6 in (8.08 m)27 ft 1 in (8.26 m)
Wing area3,554 sq ft (330.2 m2)[254]3,964 sq ft (368.3 m2)[254]
Maximum takeoff weight167,000 lb (76,000 kg)
185,000 lb (84,000 kg) (operational necessity)
204,000 lb (93,000 kg)
Cruising speedMach .86 indicated
Maximum speedMach .95 indicatedMach .93 indicated
(Mach .92 with 301 engines)
Mach .93
Service ceiling55,000 ft (17,000 m)[254]45,000 ft (14,000 m) to 56,000 ft (17,000 m)[nb 2]
Electrical system112V DC200V AC 3-phase 400 Hz
Emergency electrical
BatteryRam air turbine and Airborne Auxiliary Power Plant
Engines4 × Bristol
Olympus 101, 102 or 104
4 × Bristol
Olympus 104
4 × Bristol Siddeley
Olympus 200-series, 301
4 × Bristol Siddeley
Olympus 200-series
Fuel capacity (main)9,280 gal (74,240 lb avtur)[nb 3]9,260 gal (74,080 lb avtur)
Fuel capacity (bomb bay)None0-1990 gal (15,920 lb avtur)1990 gal[nb 4]
(15,920 lb avtur)
2985 gal[nb 5]
(23,880 lb avtur)
Powered flying controls1 x rudder (duplex), 4 x elevators, 4 x ailerons1 x rudder (duplex), 8 x elevons
Armament1 × free-fall nuclear bomb or
21 × 1,000 lb (450 kg)
conventional bombs
1 × Blue Steel missile or
1 × free-fall nuclear bomb or
21 × 1,000 lb (450 kg)
conventional bombs
  1. ^ Two extra seats could be fitted for Crew Chiefs if required, for a total of seven crew.
  2. ^ Depended upon oxygen equipment fitted. No airframe limitation on height.
  3. ^ At specific gravity of .8 (8lb/gal).
  4. ^ 2 x 995 gal cylindrical tanks.
  5. ^ 3 x 995 gal cylindrical tanks.

Popular culture[edit]

See also[edit]

Aircraft of comparable role, configuration and era
Related lists



  1. ^ RAF bombers had been traditionally named after inland towns in the British Commonwealth, or towns associated with industry.[21]
  2. ^ A contract for 25 production models had been made in July 1952. The same number of the rival Handley Page design were also ordered.[25]
  3. ^ Writing for the American Institute of Aeronautics and Astronautics, J. Seddon and E. L. Goldsmith noted that "Due to its all-wing shape, small vertical fin, and buried engines, at some angles [The Avro Vulcan] was nearly invisible to radar".[73] While writing about radar systems, authors Simon Kingsley and Shaun Quegan singled out the Vulcan's shape as acting to reduce the RCS.[74] While aviation author Doug Richardson accredits the Vulcan as having been difficult to acquire on radar, he went on to state it was unlikely to have given a great military advantage.[75] In contrast, electronic warfare author and ex-Vulcan AEO Dr Alfred Price maintains "the Vulcan [] possessed a large radar signature."[76]
  4. ^ Some B.2 aircraft armed with Blue Steel had an additional aerial plate fitted between the port tailpipes as the Blue Steel fin, in the lowered position, blanked signals from the starboard side.[84]
  5. ^ Bristol Aero Engines merged with Armstrong Siddeley in 1959 to form Bristol Siddeley which in turn was taken over by Rolls-Royce in 1966.[112]
  6. ^ According to UK parlance of the time, "megaton range" was understood to correspond to 500 kt or greater.[136] The Green Grass warhead had a predicted yield of 500 kt.[137]
  7. ^ Some sources have attested to the existence of a Vulcan B.2A. This designation supposedly referred either to Vulcan B.2s fitted with Olympus Mk 301 engines or those modified to carry the Blue Steel missile.[183][184] However, irrespective of the role or engine fit, the B.2 was the only official designation except for the MRR and tanker variants.[65][185]
  8. ^ When flying at a speed of Mach 1.0, the Vulcan suffered a position error of about 0.07.[207]
  9. ^ Avro Chief Test Pilot Tony Blackman notes that when Avro display pilots carried out aerobatics, the displays were followed by a careful but little-known inspection of the inside of the wing's leading edge. Rolls-Royce pilots also carried out aerobatics, but Blackman speculates that Rolls-Royce did not know of the inspections, and VX770 may have already been severely structurally damaged.[210]


  1. ^ Brookes and Davey 2009, p. 9.
  2. ^ "Hawker Siddeley Vulcan B2". National Cold War Exibition. Trustees of the Royal Air Force Museum. Retrieved 24 July 2013. 
  3. ^ "Hawker Siddeley Aviation Ltd." Flight, 29 August 1963, p. 342.
  4. ^ Wynn 1997, pp. 7, 16.
  5. ^ Wynn 1997, p. 18.
  6. ^ Wynn 1997, pp. 44–46.
  7. ^ Wynn 1997, p. 47.
  8. ^ a b c Gunston, W.T. "The Vulcan Story." Flight, 31 January 1958, p. 143.
  9. ^ Laming 2002, pp. 23, 24.
  10. ^ a b c Laming 2002, p. 26.
  11. ^ a b Buttler 2003, p. 31.
  12. ^ Wynn 1997, pp. 52–54.
  13. ^ Laming 2002, p. 27.
  14. ^ Laming 2002, p. 29.
  15. ^ a b Blackman 2007, p. 21.
  16. ^ Laming 2002, p. 32.
  17. ^ Blackman 2007, p. 33.
  18. ^ Laming 2002, p. 43.
  19. ^ Blackman 2007, pp. 38, 40.
  20. ^ Hamilton-Paterson 2010, pp. 18–19.
  21. ^ a b Wansbrough-White 1995, p. 44.
  22. ^ Brookes and Davey 2009, p. 8.
  23. ^ Blackman 2007, p. 41.
  24. ^ Blackman 2007, pp. 40–48.
  25. ^ Wynn 1997, p. 62.
  26. ^ Blackman 2007, p. 48.
  27. ^ a b Blackman 2007, pp. 128–129.
  28. ^ Laming 2002, p. 48.
  29. ^ Laming 2002, pp. 217–219.
  30. ^ Wynn 1997, p. 145.
  31. ^ Baxter 1990, p. 46.
  32. ^ 16,000 lb Thrust Flight 15 February 1957 p 200
  33. ^ a b Laming 2002, p. 62.
  34. ^ Wynn 1997, pp. 315, 316.
  35. ^ Wynn 1997, p. 154.
  36. ^ Wynn 1997, p. 314.
  37. ^ Laming 2002, p. 82.
  38. ^ Wynn 1997, p. 155.
  39. ^ Laming 2002, pp. 218, 219.
  40. ^ Laming 2002, p. 230.
  41. ^ Brookes and Davey, 2009, p. 12.
  42. ^ Pilot's Notes intro. Para. 1.
  43. ^ a b Pilot's Notes pt. 1, ch. 16, para. 5.
  44. ^ Laming 2002, pp. 63, 64.
  45. ^ Bulman 2001, p. 152.
  46. ^ Wynn 1997, p. 401.
  47. ^ Bulman 2001, pp. 155–161.
  48. ^ Bulman 2001, pp. 149, 150.
  49. ^ Brookes and Davey 2009, pp. 21–23.
  50. ^ Laming 2002, pp. 217–220.
  51. ^ a b c d e f g Brookes and Davey 2009, p. 83.
  52. ^ Darling 2007, p. 122.
  53. ^ a b c "Avro Type List." Avro Heritage. Retrieved: 4 August 2013.
  54. ^ a b Gibson 2011, pp. 117–118.
  55. ^ "Labour research, Volume 51." 1962, p. 20.
  56. ^ Stephens 1992, p. 142.
  57. ^ "Correspondence between the Australian and British Governments concerning the selection of the F-111 over the TSR-2." National Archives of Australia. Retrieved: 11 November 2010.
  58. ^ Weisbrod, Hanno "Australia's Decision to Buy the F-111." The Australian Quarterly, 41(2), June 1969, pp. 7–27.
  59. ^ Wilson 1989, p. 146.
  60. ^ "Falklands: FCO to MOD (sale of Vulcans to Argentina – no clearance given for sales – declassified 2012)" Margaret Thatcher Foundation. Retrieved: 4 August 2013.
  61. ^ Gunston, W. T. "Building the Vulcan." Flight, 13 December 1957, p. 926.
  62. ^ a b Pilot's Notes pt. 1, leading particulars.
  63. ^ Aircrew Manual pt. 1, ch. 2, para. 2.
  64. ^ Wynn 1997, p. 50.
  65. ^ a b Laming 2002, p. 64.
  66. ^ Pilot's Notes pt. 1, introduction, para 2.
  67. ^ Price, Blackman and Edmonson 2010, p. 102.
  68. ^ Brookes and Davey 2009, p. 65.
  69. ^ Aircrew Manual pt. 1, ch. 8, paras. 1, 2, 48.
  70. ^ Aircrew Manual pt. 1, ch. 8, paras. 3, 12.
  71. ^ Sweetman, Bill. "The Bomber that radar cannot see." New Scientist, 4 March 1982.
  72. ^ Dawson 1957, p. 3.
  73. ^ Seddon and Goldsmith 1999, p. 343.
  74. ^ Kingsley and Quegan 1999, p. 293.
  75. ^ Richardson 2001, p. 56.
  76. ^ Price, Blackman and Edmonson 2010, p. 113.
  77. ^ a b c Wynn 1997, p. 137.
  78. ^ a b Price, Blackman and Edmonson 2010, p. 112.
  79. ^ Aircrew Manual pt. 1, ch. 14, paras. 1-12.
  80. ^ Pilot's Notes pt. 1, ch. 16, para. 11.
  81. ^ a b c Price, Blackman and Edmonson 2010, pp. 102, 103.
  82. ^ Wynn 1997, p. 321.
  83. ^ Wynn 1997, p. 151.
  84. ^ Bulman 2001, p. 153.
  85. ^ Price, Blackman and Edmonson 2010, p. 106.
  86. ^ Brookes and Davey 2009, p. 57.
  87. ^ Brookes and Davey 2009, pp. 33–35.
  88. ^ Bulman 2001, p. 43.
  89. ^ Brookes and Davey 2009, pp. 36–41.
  90. ^ Bulman 2001, p. 170.
  91. ^ a b Buttler 2007, p. 72.
  92. ^ Aircrew Manual pt. 1, ch. 7, paras. 1, 7, 10, 24, 48.
  93. ^ Pilot's Notes pt.1, ch. 16, para. 1
  94. ^ Pilot's Notes pt.1, ch. 20, para. 3b
  95. ^ Pilot's Notes pt.1, ch. 16, para. 3b
  96. ^ Pilot's Notes pt. 1, ch. 10.
  97. ^ Aircrew Manual pt.1, ch. 12, para. 1.
  98. ^ "National Archive file AVIA 2347." National Archives. Retrieved: 11 September 2012.
  99. ^ Aircrew Manual pt. 1, ch. 15, p. 5.
  100. ^ Pilot's Notes pt. 1, ch. 10, para. 1(a).
  101. ^ Aircrew Manual pt. 1, ch. 7, para. 7.
  102. ^ Aircrew Manual pt. 1, ch. 7, para 70.
  103. ^ Darling 1999, p. 19.
  104. ^ Aircrew Manual pt. 1, ch. 7, para. 77.
  105. ^ Pilot's Notes, ch. 7.
  106. ^ Blackman 2007, pp. 100, 101.
  107. ^ a b Aircrew Manual, ch. 4.
  108. ^ Aircrew Manual, ch. 7.
  109. ^ a b c d e f g Laming 2002, p. 60.
  110. ^ Aircrew Manual pt. 1, ch. 10, paras. 1-3, 48.
  111. ^ Baxter 1990, p. 18.
  112. ^ Baxter 1990, p. 11.
  113. ^ Baxter 1990, p. 13.
  114. ^ "We all love the howl" Vulcan To The Sky Trust, 13 December 2013.
  115. ^ "Will 'howl' of the Vulcan bomber be heard over Bournemouth again?" The Daily Echo, 30 December 2009.
  116. ^ "Vulcan XH558 Awesome Howl Sounds" Youtube, 28 October 2012.
  117. ^ Laming 2002, pp. 45, 46.
  118. ^ Laming 2002, p. 108.
  119. ^ Laming 2002, p. 47.
  120. ^ Laming 2002, p. 63.
  121. ^ Baxter 1990, pp. 44–46.
  122. ^ Baxter 1990, p. 50.
  123. ^ "16,000 lb Thrust." Flight, 15 February 1957, p. 200.
  124. ^ Baxter 1990, pp. 50–64.
  125. ^ Lambert, C. M. "Bomex By Vulcan." Flight International, January 1958, p. 66.
  126. ^ a b c d e Blackman 2007, p. 142.
  127. ^ "Vulcans In Service: A visit to the V-force Delta of No.1 Group in Lincolnshire." Flight International, 27 September 1957, pp. 502–503.
  128. ^ a b Brookes and Davey 2009, p. 49.
  129. ^ a b c Darling 2007, p. 55.
  130. ^ Darling 2007, pp. 65, 108.
  131. ^ Mola, Roger A. "The Day Nobody Flew." airspacemag.com, November 2006. Retrieved: 5 November 2009.
  132. ^ Sgarlato, Nico. "Avro Vulcan." Aerei magazine, Delta Editions, Parma, November 1996, p. 56.
  133. ^ Darling 2007, p. 6.
  134. ^ Leitch Air Enthusiast September/October 2003, pp. 55, 58.
  135. ^ a b c d Darling 2007, p. 32.
  136. ^ Jackson Wing of Fame 1996, p. 48.
  137. ^ Leitch Air Enthusiast September/October 2003, p. 57.
  138. ^ Darling 2007, p. 19.
  139. ^ Darling 2007, p. 76.
  140. ^ a b c Brookes and Davey 2009, p. 14.
  141. ^ Brookes and Davey 2009, p. 43.
  142. ^ Brookes and Davey 2009, pp. 14–15.
  143. ^ Laming 2002, p. 88.
  144. ^ Darling 2007, p. 116.
  145. ^ Laming 2002, p. 89.
  146. ^ a b Darling 2007, p. 65.
  147. ^ Mellow, Craig (January 2004). "God Save the Vulcan!". Air & Space. Retrieved 9 September 2013. 
  148. ^ "Royal Air Force loses nuclear arsenal." AP Online, 31 March 1998.
  149. ^ Segell 1997, p. 124.
  150. ^ a b Bull 2004, p. 84.
  151. ^ Darling 2007, p. 63.
  152. ^ a b Polmar and Bell 2004, p. 261.
  153. ^ a b "The Falkland Islands: A history of the 1982 conflict." Royal Air Force, 29 April 2010.
  154. ^ Darling 2007, pp. 116–117.
  155. ^ a b c d Braybook 1982, p. 17.
  156. ^ Hearn 2007, p. 268.
  157. ^ White 2006
  158. ^ Darling 2007, p. 118.
  159. ^ Jones 2007, pp. 73–74.
  160. ^ Kev Darling, RAR Illustrated: Avro Vulcan Part 1, Big Bird Publications 2007, ISBN 978-1-84799-237-6 (p.119)
  161. ^ Chris Chant, Air War in the Falklands 1982, Osprey Publishing Limited 2001, ISBN 1841762938 (p.92)
  162. ^ Bulman 2001, p. 87.
  163. ^ Bulman 2001, p. 90.
  164. ^ "Defence." Flight International, 14 April 1979, p. 1136.
  165. ^ Frawley 2002, p. 44.
  166. ^ Halpenny 2006, p. 244.
  167. ^ a b Halpenny 2006, p. 243.
  168. ^ Darling 2007, p. 124.
  169. ^ Jackson 1990, pp. 409–411.
  170. ^ a b c Jackson 1990, p. 411.
  171. ^ Baxter 1989, p. 44.
  172. ^ Baxter 1989, p. 50.
  173. ^ Brookes and Davey 2009, p. 15.
  174. ^ Austin 2009, pp. 111–113.
  175. ^ Austin 2009, p. 113.
  176. ^ Baxter 1989, pp. 60, 64.
  177. ^ Darling 2007, p. 60.
  178. ^ Laming 2002, p. 99.
  179. ^ Brookes and Davey 2009, pp. 16–17.
  180. ^ Brookes and Davey 2009, pp. 14, 92.
  181. ^ Darling 2007, pp. 62–63.
  182. ^ a b Brookes and Davey 2009, p. 10.
  183. ^ Brookes and Davey 2009, pp. 92–93.
  184. ^ Polmar and Bell 2004, p. 262.
  185. ^ Bulman 2001, p. 154.
  186. ^ Darling 2007, pp. 122–124.
  187. ^ a b c d e f g Laming 2002, pp. 217–227.
  188. ^ Halley 2003, p. 8.
  189. ^ a b Halley 2003, p. 41.
  190. ^ Halley 2003, p. 50.
  191. ^ Halley 2003, p. 54.
  192. ^ Halley 2003, p. 63.
  193. ^ a b c d e f Jefford 1998, p. 27.
  194. ^ a b Jefford 1998, p. 28.
  195. ^ a b Jefford 1998, p. 34.
  196. ^ a b c d Jefford 1998, p. 37.
  197. ^ a b Jefford 1998, p. 39.
  198. ^ a b Jefford 1998, p. 41.
  199. ^ a b c Jefford 1998, p. 50.
  200. ^ a b c Jefford 1998, p. 54.
  201. ^ a b Jefford 1998, p. 101.
  202. ^ Lake 1999
  203. ^ a b "The Vulcan Bomber returns to the sky." BBC News, 18 October 2007.
  204. ^ "Treasury and the Basset". Flight International, 14 November 1968, p. 805.
  205. ^ Gallop 2005, pp. 114–115.
  206. ^ "Catalogue Ref. AIR 20/12396." National Archives, 1956.
  207. ^ a b Blackman 2007, p. 90.
  208. ^ "Extract from National Archives: Ref no. BT 233/403 report on crash." National Archives, Retrieved: 24 August 2010.
  209. ^ "Anniversary of Vulcan crash." BBC News, 19 September 2008.
  210. ^ Blackman 2007, p. 151.
  211. ^ a b Blackman 2007, p. 161.
  212. ^ Bak, Richard. "Mayday! Fifty years ago, a British bomber crashed into an east-side Detroit neighbourhood." Hour Detroit, July 2008.
  213. ^ Blackman 2007, p. 112.
  214. ^ http://aviation-safety.net/wikibase/wiki.php?id=59726
  215. ^ Baxter 1992, p. 60.
  216. ^ Laming 2002, p. 219.
  217. ^ a b Blackman 2007, p. 154.
  218. ^ Blackman 2007, p. 155.
  219. ^ Blackman 2007, p. 157.
  220. ^ Jackson 1990, p. 178.
  221. ^ Brookes and Davey 2009, p. 92.
  222. ^ a b Baxter 1990, p. 66.
  223. ^ Blackman 2007, p. 159.
  224. ^ "Extract from National Archives: Ref no. BT 20/12628 report on crash." National Archives. Retrieved: 24 August 2010.
  225. ^ Blackman 2007, p. 162.
  226. ^ Blackman 2007, p. 153.
  227. ^ [1]
  228. ^ "Aircraft: Vulcan B.2A." Solway Aviation Museum. Retrieved: 28 August 2010.
  229. ^ Imperial War Museum (2013). "Avro 698 Vulcan B2". IWM Collections Search. Retrieved 23 April 2013. 
  230. ^ "Avro Vulcan B2." RAF Museum. Retrieved: 28 August 2010.
  231. ^ "Avro Vulcan B2 XL319." North East Aircraft Museum. Retrieved: 28 August 2010.
  232. ^ "Latest News." Midland Air Museum. Retrieved: 28 August 2010.
  233. ^ "Vulcan B2: CFB Goose Bay." Flickr. Retrieved: 17 October 2010.
  234. ^ a b Willis 2007, p. 77.
  235. ^ "Red Arrows to Salute the Southend Vulcan." avrovulcan.com. Retrieved: 28 August 2010.
  236. ^ "Avro Vulcan B.Mk II." Strategic Air and Space Museum. Retrieved: 31 January 2015.
  237. ^ "Aircraft on display." East Midlands Airport. Retrieved: 28 August 2010.
  238. ^ "Aircraft List: Avro Vulcan B.2 XM594." Newark Air Museum. Retrieved: 28 August 2010.
  239. ^ "Vulcan bomber to be airshow draw." BBC News, 15 July 2009. Retrieved: 28 August 2010.
  240. ^ Siddeley Vulcan B2 "Hawker Siddeley Vulcan B2." National Cold War Exhibition. Retrieved: 28 August 2010.
  241. ^ "Vulcan XM603 # 1." edendale.co.uk. Retrieved: 28 August 2010.
  242. ^ "Castle Air Museum." aviationmuseum.eu. Retrieved: 28 August 2010.
  243. ^ "British bomber may soon be relic of the past." Shreveport Times. Retrieved: 28 August 2010.
  244. ^ "Avro Vulcan XM607 at RAF Waddington." Flickr. Retrieved: 28 August 2010.
  245. ^ "Avro Vulcan B.2, XM612." City of Norwich Aviation Museum. Retrieved: 28 August 2010.
  246. ^ "XM655 History." xm655.com, 3 September 2008.
  247. ^ "XH558 Vulcan Bomber first flight." youtube.com, 18 October 2007.
  248. ^ "RAF Lyneham Vulcan Cold War bomber is saved." BBC News, 25 February 2010.
  249. ^ "Vulcan bomber goes on display at Robin Hood airport." BBC News, 23 April 2011.
  250. ^ Polmar and Bell 2004, p. 264.
  251. ^ Laming 2002, pp. 155, 182.
  252. ^ Pilot's Notes AP 4505-C PN
  253. ^ Aircrew Manual AP 101B-1902-15
  254. ^ a b c Blackman 2007, p. 213.


  • Austin, Steve. "Workhorse (V-Bombers: Test-bed Vulcan)." FlyPast, No. 335, June 2009, pp. 108–113.
  • Baxter, Alan. Olympus: The First Forty Years. Derby, UK: Rolls-Royce Heritage Trust, 1990. ISBN 978-0-9511710-9-7.
  • Blackman, Tony. Vulcan Test Pilot: My Experiences in the Cockpit of a Cold War Icon. London: Grub Street, 2007. ISBN 978-1-904943-88-4.
  • Braybrook, Roy. Battle for the Falklands: Air Forces. Oxford, UK: Osprey Publishing, 1982. ISBN 0-85045-493-X.
  • Brookes, Andrew and Chris Davey. Vulcan Units of The Cold War (Osprey Combat Aircraft: 72). Oxford, UK: Osprey Publishing, 2009. ISBN 978-1-84603-297-4.
  • Bull, Stephen. Encyclopedia of Military Technology And Innovation. Santa Barbara, California: Greenwood Publishing Group, 2004. ISBN 978-1-57356-557-8.
  • Buttler, Tony. "Avro Type 698 Vulcan (Database)." Aeroplane, Vol. 35, No. 4, Issue No. 408, April 2007.
  • Buttler, Tony. British Secret Projects: Jet Bombers Since 1949. Hinckley, Leicestershire, UK: Midland, 2003. ISBN 1-85780-130-X.
  • Buttler, Tony. "Vital Bombers: Origins of the RAF's 'V-Bomber' Force". Air Enthusiast, No. 79, January/February 1999, pp. 28–41. ISSN 0143-5450.
  • Darling Kev. Avro Vulcan. North Branch, USA: Speciality Press, 1999. ISBN 1-58007-023-X.
  • Darling, Kev. Avro Vulcan, Part One (RAF Illustrated). Vale of Glamorgan Wales, UK: Big Bird Aviation Publication, 2007. ISBN 978-1-84799-237-6.
  • Dawson, T.W.G., G.F. Kitchen and G.B. Glider. Measurements of the Radar Echoing Area of the Vulcan by the Optical Simulation Method. Farnborough, Hants, UK: Royal Aircraft Establishment, September 1957 National Archive Catalogue file, AVIA 6/20895
  • Fildes, David. "Buck Rogers in the 20th Century: The Origins of the Vulcan." Aeroplane, Vol. 36, No. 3, Issue No. 419, March 2008.
  • Frawley, Gerard. The International Directory of Military Aircraft, 2002-2003. Fyshwick, ACT, Australia: Aerospace Publications, 2002. ISBN 1-875671-55-2.
  • Gallop, Alan. Time Flies: Heathrow At 60. Stroud, UK: Sutton Publishing, 2005. ISBN 0-7509-3840-4.
  • Gunston, Bill. "The V-bombers: Avro Vulcan - Part 3". Aeroplane Monthly, Vol. 8, No. 12, December 1980, pp. 620–626. ISSN 0143-7240.
  • Halpenny, Bruce Barrymore. Avro Vulcan: The History and Development of a Classic Jet. Barnsley, South Yorkshire, UK: Pen & Sword Aviation, 2006. ISBN 1-84415-426-2.
  • Hamilton-Paterson, James. Empire of the Clouds: When Britain's Aircraft Ruled the World. London: Faber & Faber, 2010. ISBN 978-0-571-24794-3.
  • Hearn, Chester G. Carriers in Combat: The Air War at Sea. London: Stackpole Books, 2007. ISBN 0-8117-3398-X.
  • Jackson, A. J. Avro Aircraft Since 1908, 2nd Edition. London: Putnam Aeronautical Books, 1990. ISBN 0-85177-834-8.
  • Jackson, Paul. "Vulcan: Delta Force". Wings of Fame, Volume 3. London: Aerospace Publishing, 1996. pp. 34–95. ISBN 1-874023-70-0. ISSN 1361-2034.
  • Jackson, Robert. Combat Aircraft Prototypes since 1945. New York: Arco/Prentice Hall Press, 1986. ISBN 0-671-61953-5.
  • Jefford, Wing Commander C.G. MBE,BA,RAF (Ret'd). RAF Squadrons:, A Comprehensive Record of the Movement and Equipment of all RAF Squadrons and their Antecedents since 1912. Shrewsbury, Shropshire, UK: Airlife Publishing, 2001. ISBN 1-84037-141-2.
  • Jenkins, Dennis R. B-1 Lancer: The Most Complicated Warplane Ever Developed. New York: McGraw-Hill, 1999. ISBN 0-07-134694-5.
  • Jones, Barry. V-Bombers: Valiant, Victor and Vulcan. Ramsbury, UK: The Crowood Press, Paperback edition, 2007. ISBN 978-1-86126-945-4.
  • Jones, Barry. "Black Buck - The Swansong." Aeroplane, Vol. 35, No. 4, Issue No. 408, April 2007.
  • Kingsley, Simon and Shaun Quegan. Understanding Radar Systems. Raleigh, North Carolina: SciTech Publishing, 1999. ISBN 1-891121-05-7.
  • Lake, Alan. Flying Units of the RAF: The Ancestry, Formation and Disbandment of all Flying Units since 1912. Shrewsbury, Shropshire, UK: Airlife Publishing, 1999. ISBN 1-84037-086-6.
  • Laming, Tim. The Vulcan Story: 1952-2002, Second Edition. Enderby, Leicester, UK: Silverdale Books, 2002. ISBN 1-85605-701-1.
  • Leitch, Andy. "V Force Arsenal: Weapons for the Valiant, Victor and Vulcan". Air Enthusiast, No. 107, September/October 2003, pp. 52–59. ISSN 0143-5450.
  • Polmar, Norman and Dana Bell. One Hundred Years of World Military Aircraft. Annapolis, Maryland: Naval Institute Press, 2004. ISBN 1-59114-686-0.
  • Price, Alfred, Tony Blackman and Andrew Edmondson. Avro Vulcan Manual: An Insight into Owning, Restoring, Servicing and Flying Britain's Legendary Cold War Bomber (Owner's Workshop Manual). Sparkford, Somerset, UK: Haynes, 2010. ISBN 1-84425-831-9.
  • Richardson, Doug. Stealth Warplanes. North Branch, Minnesota: Zenith Imprint, 2001. ISBN 0-7603-1051-3.
  • Seddon, J. and E. L. Goldsmith. Intake Aerodynamics (Aiaa Education Series). Reston, Virginia: American Institute of Aeronautics and Astronautics, 1999. ISBN 1-56347-361-5.
  • Segell, Glen. Wither or dither: British Aerospace Collaborative Procurement with Europe. London: Glen Segell Publishers, 1997. ISBN 1-901414-03-5.
  • Stephens, Alan. Power Plus Attitude: Ideas, Strategy and Doctrine in the Royal Australian Air Force, 1921-1991. Canberra, Australia: AGPS Press, 1992. ISBN 0-644-24388-0.
  • Vulcan B.Mk.1A Pilot's Notes (AP 4505C–PN). London: Air Ministry, 1961.
  • Vulcan B.Mk.2 Aircrew Manual (AP101B-1902-15). London: Air Ministry, 1984.
  • Wansbrough-White, Gordon. Names With Wings: The Names & Naming Systems of Aircraft & Engines Flown by the British Armed Forces 1878-1984. Shrewsbury, UK: Airlife Publishing Ltd, 1995. ISBN 1-85310-491-4.
  • White, Rowland. Vulcan 607: The Epic Story of the Most Remarkable British Air Attack since WWII. London: Bantam Press, 2006. ISBN 0-593-05391-5.
  • Willis, David. "Avro Vulcan survivors." Aeroplane, Vol. 35, No. 4, Issue No. 408, April 2007.
  • Wilson, Stewart. Lincoln, Canberra & F-111 in Australian service. Weston Creek, Australia: Aerospace Publications, 1989. ISBN 0-9587978-3-8.
  • Wynn, Humphrey. RAF Strategic Nuclear Deterrent Forces: Origins, Roles and Deployment 1946-1969. London: The Stationery Office, 1997. ISBN 0-11-772833-0.

Further reading[edit]

  • Arnold, Lorna. Britain And The H-Bomb. Basingstoke, Hampshire, UK: Palgrave Macmillan, 2001. ISBN 0-333-94742-8.
  • Bullman, Craig. The Vulcan B.Mk2 From a Different Angle. Bishop Auckland, UK: Pentland Press Ltd, 2001. ISBN 978-1-85821-899-1.
  • Chesnau, Roger and Ray Rimell. Avro Vulcan B Mk 2 (Aeroguide 29). Ringshall, Suffolk, UK: Ad Hoc Publications, 2003. ISBN 0-946958-39-4.
  • Dodds, Colin. "Flying the Tin Triangle." Aeroplane, Vol. 35, No. 4, Issue No. 408, April 2007.
  • Holmes, Harry. Avro: The History of an Aircraft Company. Wiltshire, UK: Crowood Press, 2004. ISBN 1-86126-651-0.
  • McLelland, Tim. The Avro Vulcan: A Complete History. Manchester, UK: Crécy Publishing Limited, 2007. ISBN 978-0-85979-127-4.

External links[edit]