| Valiant | |
|---|---|
.1_1962.png) Valiant XD873 in 1962 | |
| General information | |
| Type | Strategic bomber oraerial refueling tanker |
| Manufacturer | Vickers-Armstrongs |
| Designer | |
| Status | Retired |
| Primary user | Royal Air Force |
| Number built | 107 |
| History | |
| Manufactured | 1951–1957 |
| Introduction date | 1955 |
| First flight | 18 May 1951 |
| Retired | January 1965 |
TheVickers Valiant was a British high-altitude jetbomber designed to carry nuclear weapons, and in the 1950s and 1960s was part of theRoyal Air Force's "V bomber" strategic deterrent force. It was developed byVickers-Armstrongs in response toSpecification B.35/46 issued by theAir Ministry for anuclear-armed jet-powered bomber. The Valiant was the first of the V bombers to become operational, and was followed by theHandley Page Victor and theAvro Vulcan. The Valiant is the only V bomber to have dropped live nuclear weapons (for test purposes).[1]
In 1956, Valiants operating from Malta flew conventional bombing missions overEgypt forOperation Musketeer during theSuez Crisis. From 1956 until early 1966 the main Valiant force was used in thenuclear deterrence role in the confrontation between NATO and the Warsaw Pact powers. Other squadrons undertookaerial refuelling,aerial reconnaissance and Electronic Warfare.
In 1962, in response to advances in Soviet Unionsurface-to-air missile (SAM) technology, the V-force fleet including the Valiant changed from high-level flying to flying at low-level to avoid high altitude SAM attacks. In 1964 it was found that Valiants showed fatigue and crystalline corrosion in wing rear spar attachment forgings.[N 1] In late 1964 a repair programme was underway, but a change of Government led to the new Minister of DefenceDenis Healey deciding that the Valiant should be retired from service, and this happened in early 1965. The Victor and Vulcan V-bombers remained in service until the 1980s.
In November 1944, the Joint Technical Warfare Committee, along with a separate committee chaired by SirHenry Tizard, examined the future potential of "weapons of war" and the accompanying Tizard Report published on 3 July 1945 made specific policy directions for theRoyal Air Force (RAF)Bomber Command.[2] After theSecond World War, the policy of using heavy four-engined bombers for massed raids continued into the immediate postwar period; theAvro Lincoln, an updated version of theAvro Lancaster, became the RAF's standard bomber.[3] In 1946, theAir Staff issued Operational Requirements OR229 and OR230 for the development ofturbojet-powered heavy bombers capable of carryingnuclear weapons at high altitude and speed, without defensive armament, to act as a deterrent to hostile powers and, if deterrence failed, to perform a nuclear strike.[2] In conjunction with this ambition, Britain set about developing its ownatomic weapons.[4]
In January 1947, the BritishAir Ministry issuedSpecification B.35/46 for an advanced jet bomber intended to carry nuclear weapons and to fly near the speed of sound at altitudes of 50,000 ft (15,000 m).[5] Three firms:A.V. Roe,Handley-Page andVickers-Armstrongs submitted advanced designs intended to meet the stringent requirements.[6] WhileShort Brothers submitted a design, byGeoffrey T. R. Hill,[7] that was judged too ambitious, the Air Staff accepted another submission from the company for a separate requirement, B.14/46, as "insurance" in case the advanced B.35/46 effort ran into trouble. Aviation authors Bill Gunston and Peter Gilchrist described Specification B.14/46 as "calling for little more than a traditional aircraft fitted with jet engines"[8] Short submitted a conservative design to meet B.14/46, which became theS.A.4 Sperrin.[5] Two prototypes were completed, the first conducting itsmaiden flight in 1951, but the Sperrin was ultimately relegated to research and development purposes only.[6][4]
Vickers had emerged from World War II as one of the world's pre-eminent companies in the field of aeronautical manufacturing and development. The company operated its own secretiveSkunk Works-like development organisation based at Weybridge, Surrey, which had been involved in several secret wartime development projects. It was this secretive division where the early development of the Valiant took place, including the later assembly of the initial two prototypes.[9] Vickers initially produced a six-engine jet bomber design proposal to meet Specification B.35/46. As progress in the development of more powerful jet engines was made, this was re-worked to a four-engine proposal in 1948.[10] The proposed design submitted by Vickers was relatively straightforward, being less aerodynamically advanced in comparison to competing bids made by rival firms.[8][11]
Both Handley-Page and Avro had produced advanced designs for the bomber competition. These were produced as theVictor and theVulcan respectively. The Air Staff decided to award contracts to each company as a form of insurance in case one of the designs failed. The submissions became known as theV bombers, or V-class, with the aircraft given names that started with the letter "V".[12] Vickers' submission had initially been rejected as not being as advanced as the Victor and the Vulcan,[5][8] but Vickers' chief designerGeorge Edwards lobbied the Air Ministry on the basis that it would be available much sooner than the competition, going so far as to promise that a prototype would be flown by the end of 1951, that subsequent production aircraft would be flown prior to the end of 1953, and that serial deliveries would commence during early 1955. Gaining the bomber contract was considered of crucial importance to the future of aircraft manufacturing at Vickers.[10] "Edwards was supremely confident that Weybridge could deliver the aircraft as specified .. " and "..committed to the brochure performance figures and dates because he thought they knew how to do it". He resisted being pushed to try to more closely match the Victor and Vulcan height and speed requirements or to change equipment from that originally specified as these distractions would jeopardize his promised delivery dates.[13]
Although developing three different aircraft types in response to a single Operational Requirement (OR) was costly, events such as theBerlin Blockade had led to a sense of urgency in providing a deterrent to the Soviet Union from possible acts of aggression in Western Europe.[14][8]
In April 1948, the Air Staff issued a specification with the designation B.9/48 written around the Type 660 Vickers design; and an 'Instruction to Proceed' was received by Vickers on 16 April 1948.[10]
In February 1949, two prototypes of the Vickers 660 series were ordered. The first was to be fitted with fourRolls-RoyceRA.3 Avonturbojet engines, while the second was to be fitted with fourArmstrong Siddeley Sapphire engines and was designated the Type 667.[15]
On 18 May 1951, the first prototype,serial number WB210 took to the air for its maiden flight,[16] within the deadline that George Edwards had promised, only 27 months since the contract had been issued. This was several months before the competing Short Sperrin; the Sperrin had straight (not swept) wings and was not ordered. The Valiant pilot wasCaptain Joseph "Mutt" Summers, who had also been the original test pilot on theSupermarine Spitfire, and wanted to add another "first" to his record before he retired. His co-pilot on the first flight was Gabe "Jock" Bryce, who succeeded Summers as Vickers' chief test pilot upon his retirement shortly after.[17][18][19] The next month, the Vickers Type 660 was given the official name of "Valiant", reusing the name given to theVickers Type 131 general-purpose biplane of 1931.[N 2] The name Valiant had been selected by a survey of Vickers employees.[20]
On 11 January 1952, the first Valiant prototype was lost while making internal noise measurements for theV.1000 programme. Testing included engine shutdowns and re-lights,[21] one of which caused a fire in the starboard wing; most of the crew managed to escape the aircraft safely, except for the co-pilot, who struck the tail after ejecting.[22][23]
On 11 April 1952, the second prototype WB215 made its maiden flight, after modifications to the fuel system.[24] It was fitted with more powerful RA.7 Avon engines with 7,500 pounds-force (33 kN) thrust each, rather than the originally planned Sapphires. It also featured more roundedair inlets, replacing the narrow slot-type intakes of the first prototype, to feed sufficient air to the more powerful engines. The short delay until the second prototype became available meant that loss of the prototype did not compromise the development schedule.[25][26][11]
One of the three prototypes was the B.2 version.[27] The B.2 was intended to serve as aPathfinder aircraft, flying at low level to mark targets for the main bomber force. To cope with increased air turbulence at low level, the B.2 had a strengthened airframe. In particular, the wing was strengthened with the removal of the cut-outs in the wing structure into which the main wheels retracted, allowing the wing torsion box structure to be uninterrupted and giving more room for internal fuel storage. Instead, the main landing gear, which had four wheels instead of the two wheels of the B.1, retracted backwards into largefairings set into the rear of the wings.[28] The B.2 had a lengthened fuselage with a total length of 112 ft 9 in (34.37 m), in contrast to a length of 108 ft 3 in (32.99 m) for the Valiant B.1, with the extra length giving room for more avionics.[29]
The prototype B.2, serial number WJ954 first flew on 4 September 1953.[30] Finished in a gloss black night operations paint scheme, it became known as the "Black Bomber". Its performance at low level was superior to that of the B.1 (or any other V-bomber), particularly atsea level,[31] with the aircraft being cleared for 580 mph (930 km/h) at low level (with speeds of up to 640 mph (1,030 km/h) being reached in testing). This was compared to the B.1 sea-level limit of 414 mph (665 km/h). The Air Ministry ordered 17 production B.2 aircraft, which were to be powered byRolls-Royce Conwayturbofans. Although the Valiant B.2 low-level capabilities were significant, the programme was terminated because the World War 2 "Pathfinder concept" was considered obsolete in the nuclear era.[32] The B.2 prototype was used for tests for a few years, including the clearance of rocket-assisted take-offs, for the Valiant B.1 at hot or high airfields, using two Super-Sprite rocket motors. It also did extensive taxiing tests to investigate the cause of brake judder which caused a fatigue failure of the landing gear. It was scrapped in 1958.[33][34][35][36]
In April 1951, an initial production order for 25 Valiant B.1 (Bomber Mark 1) aircraft was placed by the Ministry of Supply on behalf of the RAF.[37] The timing of this order was key to establishing production quickly. Due to shortages ofsteel and other materials while setting up an assembly line at Brooklands, substantial portions of the productionjigs for the Valiant were made fromconcrete.[31] The first five Valiants produced were completed to a pre-production standard, the first being WP199. On 21 December 1953, the production aircraft conducted its first flight; this had again occurred within the schedule that Edwards had promised.[38][31]
On 8 February 1955, this first production Valiant was delivered to the RAF.[39][4] Britain's "V-bomber" force, as it had been nicknamed in October 1952, formally entered operational service on that day. The Victor and Vulcan would soon follow the Valiant into service, for a total of three types of nuclear-armed strategic bombers in RAF service. In September 1957, the final Valiant was delivered.[40] All production aircraft had been delivered on time and below budget.[32]
A total of 108 Valiants were manufactured, including the sole B.2 prototype. In addition to its principal role as part of Britain'snuclear deterrent, the Valiant bomber also dropped high explosive bombs. The bombers were followed into service by a strategic reconnaissance version and a multi-purpose version capable conventional bombing,aerial reconnaissance andaerial refuelling. 18 squadron operated 6 Valiants withelectronic countermeasures equipment.[41] Valiants of 90 and 214 squadrons were used for air refuelling through the addition of a Hose Drum Unit (HDU) in the bomb bay, mounted on the same suspension units that were also used for bombs. This meant that for refuelling, the bomb-bay doors had to be opened so that the refuelling hose could be streamed (unlike later tankers where the HDU was flush with the under fuselage rather than inside a bomb bay). Several Valiants were also used for testing and development purposes, such as its use as a flying testbed during trials of theBlue Steel nuclear-armedstandoff missile, which was later added to the arsenal of munitions the other V-bombers were equipped with.[42][43]
Unlike the Vulcan and Victor, the Valiant did not see the production of a more capable mark 2 model.[4] In 1962 the Valiant bomber squadrons were switched to a low-level flight profile in order to avoid enemy Surface-to-Air (SAM) defence systems. In 1964fatigue was discovered due to the increased air turbulence in low level flying and led to the type's premature retirement. Vic Flintham observed that: "There is a fine irony to the situation, for Vickers had produced the Type 673 B Mk 2 version designed as a fast, low-level pathfinder... The Air Ministry was not interested..."[43] The Valiant was Vickers' last purpose-built military aircraft. It was followed by theVanguard, a passenger turboprop designed in 1959, and theVickers VC10, a jet passenger aircraft in 1962, also used as a military transport and tanker by the RAF.[4]
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The Valiant was based on contemporary aeronautical knowledge with no advanced untried aerodynamics that required proving with scaled-down research aircraft or lengthy research and development. As a result George Edwards described the Valiant[44] as an "unfunny" aircraft.The Valiant had a shoulder-mounted wing and four Rolls-Royce Avon RA.3 turbojet engines, each providing up to 6,500 pounds-force (29 kN) of thrust, installed in pairs infireproof bays in each wing root.[45] The design of the Valiant gave an overall impression of a clean aircraft with swept-wing aerodynamics.[46] The root chord thickness ratio of 12% allowed the Avon engines to be within the wing rather than on pods as in the contemporaryBoeing B-47.[47] This "buried engine" installation contributed to the aircraft's aerodynamic cleanness, and was British practice at the time. It made engine access for maintenance and repair difficult and increased the risk that an uncontained failure of one engine would cause damage to the adjacent engine; it also increased the complexity of the design of the main spar which had to be routed around the engines.[48]
The wing of the Valiant used a "compound sweep" configuration, devised by Vickersaerodynamicist Elfyn Richards.[49] Richards found that it was necessary to increase the sweep on the inboard section of the wing, a discovery which he laterpatented as "Improvements in Aeroplane Wing Formation" with an explanation that "the formation of the shockwaves be delayed to the same extent over the whole span of the wing";[50] the Valiant wing had 37° sweepback for the inner third of the wing, and 21° for the remainder.[51][52] This was because the thickness/chord ratio could be reduced closer to the tips.[49] The choice to have mild sweepback around the aerodynamic control surfaces meant that in-service speeds were limited to Mach 0.84 and a typical cruise of Mach 0.75 at heights up to 55,000 feet (17,000 m) when lightly loaded.[53][54] Adrogue parachute was not necessary even operating from runways as short as 6,000 feet (1,800 m).[31]
The wing was mounted high on the fuselage and the location of the engines and mainlanding gear within the wing limited the volume available for fuel.[45] Thetrailing edge of the wing had two-sectionailerons withtrim tabs, and inboard of the ailerons were double-slottedflaps.[55] Directelectrical drives were used to move the flaps and landing gear. The only hydraulically-operated equipment, the steering and brakes, was also powered by electric motors but driving hydraulic pumps instead of mechanical gearing.[56]
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Production aircraft were powered by four Avon 201 turbojet engines, with 9,500 pounds-force (42 kN) thrust. The engines also providedbleed air for thepressurization,ice protection, andair conditioning systems. The aircraft's DC electricalgenerators were also driven by the engines.[56]Napier Spraymatelectric heaters were installed in the engine inlets to prevent ice formation and subsequent shedding possibly causing engine damage. The shape of the engine inlets were long rectangular slots in the first prototype, whereas production Valiants had oval or "spectacle" shaped inlets designed to pass greater airflow for the more powerful engines that were installed.[47] The jet exhausts emerged from fairings above the trailing edge of the wings.[47]
For required takeoff performance from short tropical dispersal bases,[57] ajettisonablerocket booster engines pack was developed for the Valiant.[32] Trials were performed with two underwingde Havilland Sprite boosters; they were no longer needed when more powerful variants of the Avon engine became available. Also, there was an increased risk of accidents if one booster rocket failed on takeoff, resulting in asymmetric thrust.[36] Some Valiant engines hadwater injection, which increased takeoff thrust by about 1,000 pounds-force (4.4 kN) per engine.[58]
The crew were in a pressurized compartment in the forward fuselage and consisted of a pilot, co-pilot, two navigators, and air signaller (later called an air electronics officer (AEO)).[59] Manufacture of this pressurized section was subcontracted toSaunders-Roe. The pilot and co-pilot were located side by side on an upper level, the remaining three crew members sat at stations lower in the cockpit, and faced to the rear.[60] The crew was reduced to five with the deleted requirement for defensivegun turrets andair gunners, an operational philosophy proved by theDe Havilland Mosquito bomber of World War II.[52][N 3] The pilot and copilot were provided withMartin-Baker Mk.3ejector seats, while the rear crew had to bail out of the oval main entrance door on the port side of the fuselage.[61] Safe escape using this exit was not considered likely.[45]
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The fuselage area behind the pressurised crew section and forward of the wing was used to house much of theavionics, and air conditioning equipment, and was sometimes called the "organ loft".[45] The Valiant had twin-wheel nosegear andtandem-wheel main gear that retracted outwards into recesses in the underside of the wing. Each of the main gears were equipped with multipadanti-skiddisc brakes, and weretelescopically linked so that a single drive motor could pull them up into the wing recesses.[45] Most of the aircraft systems were electric, including the flaps and undercarriage.[62] The brakes and steering gear were electrically powered, driving hydraulic pumps for actuation.[63][64] The lower half of the aircraft nose contained the scanner for theH2Sradar in aglass fiberradome; in addition, a visualbomb sight was located beneath the lower floor of the pressurised cockpit.[45] The avionics bay was not accessible from the cockpit but could be accessed using an entrance at the base of the rear fuselage leading to an internalcatwalk above the aft part of thebomb bay.[65]
The electrical systems used 112 voltdirect current generators, one on each engine, for functions requiring large amounts of electrical power. A 28 V DC system was used for other uses including actuators that controlled the higher-voltage system functions. Backup power came from 24 V and 96 V batteries. 115 Valternating current was provided for the radar and theactuators for the flight surfaces, flaps,air brakes and undercarriage.[63][66][64] It was decided during the design phase that as much of the aircraft would be electrically driven as was possible; the complete electrical system including high voltage generators and cabling, together with electric motors with mechanical drives, was lighter than the hydraulic equivalent consisting of pumps, tubing, actuators, fluid and storage tanks.[56]
Theflight controls of the Valiant (ailerons, elevator and rudder) consisted of two channels of power control with full manual backup; flying in manual was practised during training as it would be required if a complete electrical failure occurred during a flight.[63] In "manual" the flight controls required considerable physical effort to operate.[64] The pilot's controls for elevators, ailerons and rudder had anartificial feel system, the pressure for which was provided from aram-air inlet.[56]
ASmith Aerospaceautopilot andinstrument landing system (ILS) was installed along with variousnavigational aids, such as theMarconi Company-builtGreen Satindoppler radar,Geeradio navigation,Automatic Direction Finder (ADF),VOR/Distance Measuring Equipment (DME), andradar altimeters.[31] Provisions for additional equipment and sensors, such asside looking airborne radar, were also made.[31]
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The centre fuselage of the Valiant had a main backbone beam to support the weight of the two widely-setwing spars and fivefuel cells in the upper fuselage. The bomb bay was also in the lower half of the centre fuselage.[45][67] The aft fuselage used asemi-monocoque structure, being lighter than the centre fuselage; theBoulton-Paul-produced electro-hydraulic power units for the ailerons,elevators, andrudder were contained within this space.[56] The tail, which was attached to the rear fuselage wastapered rather than swept back,[45] thehorizontal tailplane was mounted well up thevertical fin to keep it clear of the engines' exhaust.[49] The tailcone contained an ARI 5800 Orange Puttertail warning radar.[32]
The main structural components, spars and beams of the Valiant had been constructed from a zinc/magnesium/copper aluminium alloy called DTD683 in the UK.[68][69] The Valiant had been designed with a 'Safe-Life' strategy;[70] this combination of 'Safe-Life' and DTD683 came to be viewed as a severe mistake. In 1956, a publication within the Journal of the Institute of Metals[71][N 4] condemned the material DTD683 as being unstable and capable of catastrophic failure when stressing the airframe close to its design limits. The "Safe-Life" design strategy was dismissed by a Lockheed engineer in a talk given to theRoyal Aeronautical Society in 1956, because it did not guarantee safety from catastrophic failure.[72]
The Valiant B.1 could carry a 10,000-pound (4,500 kg) nuclear weapon or up to 21 1,000 lb (450 kg) conventionalbombs in its bomb bay. It was designed for the earlyfission-based nuclear weapons and also the newer and largerthermonuclearhydrogen bombs.[45] A "clean" Valiant (one without underwing tanks) could climb straight to 50,000 ft after takeoff unless it had heavy stores in the large bomb bay.[citation needed]
In the aerial reconnaissance role, a camera crate would be installed in the bomb bay, along with a pair of cameras set into the fuselage and larger rear fuel tanks to extend the aircraft's endurance.[73] Large external fuel tanks under each wing with a capacity of 1,650 imperial gallons (7,500 L), could be used to extend range; an auxiliary fuel tank could also be installed in the forward area of the bomb bay; the external wing tanks were fitted as standard on Valiants that were operated as aerial refuelling tankers.[73] For receiving fuel, a fixedrefuelling probe was fitted onto the aircraft's nose, this was connected to the fuel tanks via a pipe running along the outside of the canopy to avoid penetrating the pressure cabin.[74]
The first squadron to be equipped with the Valiant was138 Squadron, which formed atRAF Gaydon on 1 January 1955, with 232 Operational Conversion Unit forming at Gaydon on 21 February 1955 to convert crews to the new bomber.[75] Since the Valiant was part of an entirely new class of bombers for the RAF, the crews for the new type were selected from experienced aircrew, with first pilots requiring 1,750 flying hours as an aircraft captain, with at least one tour flying the Canberra, with second pilots needing 700 hours in command and the remaining three crewmembers had to be recommended for posting to the Valiant by their commanding officers.[76] Valiants were originally assigned to the strategic nuclear bombing role, as were the Vulcan and Victor B.1s when they became operational. At its peak, the Valiant equipped ten RAF squadrons.[77][78]
According to Gunston and Gilchrist, the Valiant had performed "extremely well" during the annual bombing competition hosted by AmericanStrategic Air Command (SAC).[74] American interest in the Valiant resulted in a visit to Vickers by USAF generalsVandenberg, Johnson andLeMay. Vickers test-pilot Brian Trubshaw believed that George Edwards was put under some pressure to build the Boeing B-47 under license. The only result from the visit was Le May's insistence that the Valiant pilot side-by-side seating be incorporated in the B-52 instead of the tandem arrangement in the B-47 and prototype B-52.[79]
On 11 October 1956, a Valiant B.1 (WZ366) ofNo. 49 Squadron piloted byEdwin Flavell was the first British aircraft to drop an atomic bomb when it performed a test drop of a down-ratedBlue Danube weapon onMaralinga,South Australia.[80] This occurred as part of theOperation Buffalonuclear tests in that area. Windscreen blinds were fitted in advance of the test to protect the crew from the intense flash of light from the nuclear detonation. Following the landing of the aircraft after deploying the weapon, WZ366 was assessed for potential damage and forradioactive contamination.[81]
On 15 May 1957, a Valiant B(K).1 (XD818) piloted byKenneth Hubbard dropped the first British hydrogen bomb, the Short Granite, over the Pacific as part ofOperation Grapple.[82] No 49 Squadron was selected to perform the live weapon drop, and were equipped with specially-modified Valiants to conform with the scientific requirements of the tests and other precautionary measures to protect against heat and radiation.[83] However, the measured yield was less than a third of the maximum expected although achieving a thermonuclear explosion.
On 8 November 1957 a British hydrogen bomb detonated with its planned yield in the Grapple X test.[84] The Grapple series of tests continued into 1958, and in April 1958 the Grapple Y bomb exploded with ten times the yield of the original "Short Granite".[85] Testing was finally terminated in November 1958, when the British government decided it would perform no more air-delivered nuclear tests.[74]
Originally the bombing role was to have been carried out at high altitude, but following the shooting down in 1960 of theLockheed U-2 flown by Gary Powers by an early SovietSA-2 Guideline missile, the SAM threat caused bomber squadrons to train for low-level attack as a means of avoiding radar detection when flying within hostile airspace. They were repainted in grey/green camouflage with normal markings, replacing theiranti-flash white scheme.[43] By 1963, four Valiant squadrons (49, 148, 207 and 214) had been assigned toSACEUR in the low-level tactical bombing role.[74] By this point, there had been a noticeable decline in flying rates for the type.[74]
Peacetime practice involved the dropping of small practice bombs on instrumented bombing ranges, and a system of predicted bombing using radio tones to mark the position of the bomb drop over non-range targets, the bomb error being calculated by a ground radar unit and passed either to the crew during flight or to a headquarters for analysis. Use of the Valiant's Navigational and Bombing System (NBS) and the high quality of assigned crews, who were typically veterans and often had been previously decorated for wartime service, meant a high level of bombing accuracy could be achieved, greater than that of aircraft during the Second World War. According to Gunston and Gilchrist, Valiant crews were able to place practice bombs from an altitude of 45,000 feet (14,000 m) within a few meters of their assigned target.[74]
In October and November 1956 the Valiant was the first of the V-bombers to see combat, during the Anglo-French-Israeli Suez campaign. DuringOperation Musketeer, the British military operation in what became known as theSuez Crisis, Valiants operating from the airfield at Luqa on Malta dropped conventional bombs on targets inside Egypt. Egyptian military airfields were the principal target; other targets included communications such asradio stations and transport hubs.[86] On the first night of the operation, six Valiants were dispatched to bombCairo West Air Base (which was aborted in flight due to potential risk to US personnel in the vicinity) while six more attackedAlmaza Air Base and a further five bombedKibrit Air Base and Huckstep Barracks.[87][88]
Although the Egyptians did not oppose the attacks and there were no Valiant combat losses, the results of the raids were reported as disappointing. Although the Valiants dropped a total of 842 long tons (856 t) of bombs, only three of the seven airfields attacked were seriously damaged.[N 5] The Egyptian Air Force had been effectively destroyed in a wider series of multinational attacks of which the Valiant bombing missions had been a part.[89] It was the last time RAF V-bombers flew a live combat mission until Avro Vulcans bombed Port Stanley airfield in the Falkland Islands during theFalklands War in 1982.[90]
Valiant tankers were flown by No. 214 Squadron atRAF Marham, operational in 1958, and No. 90 Squadron at Honington, operational in 1959.[40] The two squadrons became dedicated tanker squadrons on 1 April 1962.[91] Aircraft assigned to the tanker role were fitted with a Hose Drum Unit (HDU or "HooDoo") in the bomb bay. The HDU was mounted on bomb-mounting points and could be removed, so that the aircraft could be reverted to the bomber role if required;[92] this arrangement meant that the bomb bay doors had to be opened in order to transfer fuel to a receiver aircraft. A control panel at the radar navigator station in the cockpit was used to operate the HDU.
Long-range demonstration flights were made with in-flight refuelling by other Valiant tankers that had been positioned at airfields along the route. In 1960, a Valiant bomber flew non-stop from Marham in the UK to Singapore and in 1961 a Vulcan flew non-stop from the UK to Australia.[40] The two tanker squadrons regularly made long range flights. These included non-stop flights from the UK toNairobi,RAF Gan andSingapore.[93] Other aircraft refuelled by Valiants at this time included Victor and Vulcan bombers,English Electric Lightning fighters, andde Havilland Sea Vixen andSupermarine Scimitar fighters of the Royal Navy.[94]
Valiants ofNo. 18 Squadron RAF atRAF Finningley were modified to the "radio countermeasures" (RCM) role—now called "electronic countermeasures" (ECM). These aircraft were ultimately fitted with American APT-16A and ALT-7 jamming transmitters,Airborne Cigar and Carpetjammers, APR-4 and APR-9 "sniffing" receivers, andchaff dispensers. At least seven Valiants were configured to the RCM role.[95]
Valiants of No. 543 Squadron atRAF Wyton were modified to serve in the photographic reconnaissance role. In one notable operation in 1965, Valiants of No. 543 Squadron photographed around 400,000 square miles (1,000,000 km2) ofRhodesia across an 11-week period.[40]
In 1956, Vickers had performed a series of low level tests in WZ383 to assess the type for low level flight at high speed. Several modifications to the aircraft were made, including a metal radome, debris guards on the two inboard engines, and after six flights the aileron and elevator artificial feel was reduced by 50%. Pilots reported problems with cabin heating and condensation that would need remedying. The aircraft was fitted with data recording equipment and these data were used by Vickers to estimate the remaining safe life of the type under these flying conditions. Initially a safe life of 75 hours was recommended, which became "the real figure might be less than 200 hours".[96] The number of hours flown by each Valiant in a year was an operational issue for the RAF.[97]
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Later theRAE ran a similar series of tests that more closely resembled actual operational conditions including low level and taxiing; the corresponding report published in 1958 produced data that could be used to get a better grasp on which flight conditions produced the most damage, and enable a better projection of the future life span for the type.[98]
In May 1957Flight reported an "incident at Boscombe Down, when the wing rear spar cracked after a rocket-assisted takeoff at overload weight (the reason for the rocket-assistance)"[99] This aircraft was the second prototype WB 215 and had not been modified with the production fix for the known weakness in the rear spar;[100] the aircraft was subsequently broken up for wing fatigue testing after it had flown 489 hours.[101]
After years of front-line service, in July 1964, a cracked spar was found in one of the three Valiants (either WZ394 – Wynne, or WZ389 – Morgan) on Operation Pontifex.[102] This was followed on 6 August by a failure of the starboard wing rear spar at 30,000 ft,[103] in WP217, an OCU aircraft from Gaydon captained by Flight Lieutenant "Taffy" Foreman. The aircraft landed back at Gaydon but without flap deployment because damage to the starboard rear spar caused the flap rollers to come out of their guides so that the flap would not lower on that side. Later inspection of the aircraft also showed the fuselage skin below the starboard inner plane had buckled, popping the rivets; the engine door had cracked and the rivets had been pulled and the skin buckled on the top surface of the mainplane between the two engines.[104] Both of these aircraft were PR variants.[105]
Inspections of the entire fleet showed that the wing spars were suffering from fatigue at between 35% and 75% of the assessed safe fatigue life, probably due to low level turbulence.[75] After this inspection, the aircraft were divided into three categories, Cat A aircraft continuing to fly, Cat B to fly to a repair base, and Cat C requiring repair before flying again. The tanker squadrons had the highest proportion of Cat A aircraft because their role had been mainly at high level.[75] This also caused the methods of assessing fatigue lives to be reviewed.[106] By the time the type was scrapped, only about 50 aircraft were still in service; the rest had been slowly accumulating at various RAF Maintenance Units designated as "Non effective Aircraft".[107]
Initially there was no question of retiring the type, or even a majority of affected aircraft. Repairs were actively taking place at Valiant bases such as Marham using working parties from Vickers plus RAF technicians from the base. In January 1965, the Wilson government withDenis Healey asSecretary of State for Defence decided that the expense of the repairs could not be justified, given the short operational life left to the Valiant, and the fleet was permanently grounded as of 26 January 1965.[108] The QRA alert that had been in place forSACEUR was maintained until the final grounding.[109] When asked to make a statement regarding the Valiant's scrapping in theHouse of Commons, Denis Healey stated that it "was not in any way connected with low-level flying" and that the "last Government took the decision to continue operating the Valiant force for another four years after its planned fatigue life was complete".[110]
Aviation author Barry Jones commented in his book that: "A question has to be asked. For two years before the demise of the Valiant, Handley Page at Radlett had 100Hastings go through their shops. They were completely dismantled and rebuilt, having DTD683 components removed and replaced by new alloy sections. What was so special about the Hastings and why was the Valiant not treated similarly? Perhaps we will know one day – but I doubt it."[111] AFlight report about the scrapping states "Fatigue affected all Valiants ... not only those that had been used for some low flying".[112]
On 9 December 1964, the last Valiant tanker sortie in XD812 of 214 Squadron was refuelling Lightning aircraft over the North Sea and was recalled to land back at Marham before the scheduled exercise was completed. On the same day, the last Valiant bomber sortie was carried out by XD818.[N 6]
Including the three prototypes, a total of 107 Valiants were built.[113][114]
Valiant production ended in August 1957.[114] An order for 17 B.2 models was cancelled.[115]
Data fromVickers Aircraft since 1908,[130]Jet Bombers[131]
General characteristics
Performance
Armament
Aircraft of comparable role, configuration, and era
Related lists
| External videos | |
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 Newsreel footage of Valiant following 1955 Speed Record | |
| Footage and Description of the Valiant B2 | |
| Period footage of RAF Valiant operations | |
| High Encounter |
| International | |
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| National | |
| Other | |
