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The Handley Page Victor

v1.1.4 / 01 jun 16 / greg goebel

* In the 1950s, the British Royal Air Force (RAF) acquired a strategic nuclear strike force in the form of the "V-Bombers" -- the Vickers Valiant, the Handley Page Victor, and the Avro Vulcan. The Victor was arguably the most unconventional of the three, at least in hindsight, but it proved very successful, persisting in service into the 1990s in the tanker role. This document provides a history and description of the Victor.

Handley Page Victor prototype


[1] VICTOR ORIGINS
[2] VICTOR B.1 & B.1A
[3] VICTOR B.2 & SR.2
[4] VICTOR TANKERS
[5] VICTOR IN ACTION
[6] SUMMARY, COMMENTS, SOURCES, & REVISION HISTORY

[1] VICTOR ORIGINS

* The Handley Page Victor was the last of the three British V-bombers to enter service. It was submitted in response to the same 1946 British Air Ministry requirement for a nuclear strike platform that gave rise to the Avro Vulcan, B.35/46, though Handley Page had already been considering concepts for some time and the basic design, designated "HP.80", was in hand when the requirement was issued.

The HP.80 was intended to operate at high speed and altitude, above the ceiling of contemporary fighters. The aircraft featured a "crescent" wing, with the sweep decreasing in three steps -- 48.5 degrees to 37.5 degrees to 26.75 degrees -- from the root to the tip, and the chord similarly decreasing to ensure a constant limiting Mach number across the entire wing, and a high cruise speed.

The HP.80 had its roots in wartime design work performed by Dr. Gustav Victor Lachmann, a German national who had been working for Handley Page when war broke out and had been interned. Handley Page was eventually able to prevail on the authorities to let Lachmann continue work for the company, in cooperation with his deputy, Godfrey Lee. Just after the end of the war, Lee went to Germany to learn about German advanced aircraft research; when he returned to England he came up with the crescent-wing design, while bedridden with pneumonia. Incidentally, the Germans had designed a similar crescent wing for an improved version of the Arado Ar-234 jet bomber, but it doesn't appear that Lee saw any of the plans for it during his visit to Germany. In any case, the company liked Lee's concepts. He later said: "Perhaps we were the only firm brave enough or daft enough to do it." The Air Ministry also thought the idea had merit, and authorized construction of two prototypes in April 1948.

* The HP.80's crescent wing was to be tested on a one-third scale radio-controlled glider, designated the "HP.87", but it crashed on its first flight. This exercise having proven a failure, in 1948 the Air Ministry issued another specification, "E.6/48", for a piloted demonstrator, which emerged as the "HP.88".

HP.88 design and construction was farmed out to General Aircraft LTD. General Aircraft obtained a fuselage for the Attacker jet fighter from Supermarine, then refitted it with a crescent wing and a tee tail. The HP.88 performed its first flight on 21 June 1951. General Aircraft had been bought out by Blackburn by this time, and Blackburn test pilot G.R.I. Parker was at the controls.

Handley Page HP.88

However, the HP.80's design had changed in the interim, and the HP.88 wing was no longer representative of the aircraft it was supposed to be testing. In addition, the initial HP.80 prototype was already under construction; to make the HP.88 a completely dreadful exercise in futility, it broke up in flight on 26 August 1951, killing the pilot, D.G. "Duggie" Broomfield.

* WB771, the first of the two HP.80 prototypes, was hauled by road 145 kilometers (90 miles) from the Handley Page factory at Radlett to the test center at Boscombe Down for flight trials. There was a runway at Radlett and the original expectation had been that test flights would take place there, but the government decided that the longer runway at Boscombe Down would provide an additional margin of safety.

The transfer of the aircraft was a substantial project in itself. The route had to be scouted out for clearance, with alterations made by bulldozer to the terrain alongside two curves, and then the aircraft was broken down and packed up. The fuselage was disguised with some wood framing before it was wrapped, and the words "GELEYPANDHY / SOUTHHAMPTON" were stenciled on the covering, as if it was some sort of boat being taken to harbor for launch. GELEYPANDHY, incidentally, was supposed to be an anagram of "Handley Page", but either through clumsiness or a desire to conceal the clue, it actually sorted out to "Handley-Pyge".

WB771 was reassembled at Boscombe Down. While the aircraft was being run through ground hydraulic tests preparatory to the initial flight, a fire broke out and doused three techs with burning hydraulic fluid, one of them dying in the hospital a few weeks later. WB771 was finally put into condition for taking to the air, and the prototype performed its initial flight on 24 December 1952, with Handley Page's chief test pilot, Squadron Leader Hedley George Hazelden, at the controls. WB771 was powered by four Armstrong Siddeley Sapphire 7 Mark 200 turbojet engines. It was not fitted with operational kit, ballast being used to achieve flight trim. Hazelden described the initial flight as "comfortable", with "no anxieties". The takeoff run was surprisingly short; there had been no real need to move the machine to Boscombe Down.

Handley Page HP.80 prototype

WB771 made an appearance at the Farnborough Air Show in 1953, with the aircraft painted in spiffy colors -- black fuselage with a red cheatline and silver flight surfaces. Trials showed the basic design to be sound, with some corrections needed. Unfortunately, one of the corrections was discovered very much the hard way, when WB771 was lost in a crash on 14 July 1954 while on a low-level run. The tail assembly was weak and tore off, with test pilot Ronald Ecclestone and his crew all killed.

* The second prototype, WB775, which featured a reinforced tail, performed its initial flight on 11 September 1954. It had the same spiffy color scheme that had been applied to the first prototype, and actually took a joyride to the Farnborough air show during the initial flight. It was fitted with operational kit.

Production of the HP.80 had been ordered in June 1952, well before the first flight of the initial prototype, with the British Air Ministry ordering a batch of 25 production bombers, to be designated "Victor B.1". First flight of a production aircraft was on 1 February 1956, with test pilot Johnny Allam at the controls. Allam "accidentally" broke Mach 1 in a shallow dive on 1 June 1957, making it the largest aircraft to that time to exceed the speed of sound.

Service trials stretched out, with fixes piling up and leading to delays. The type finally entered RAF service with Number 232 Operational Conversion Unit (OCU) in November 1957, and reached its first operational unit, RAF Number 10 Squadron, in April 1958.

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[2] VICTOR B.1 & B.1A

* The Victor was an aerodynamically clean aircraft, with very exotic and absolutely unique "the future as seen by the past" lines. It was made mostly of aluminum aircraft alloys, in the form of a two-skin sandwich with corrugated filling, held together with spot welding. The wing had large rear flaps and leading-edge flaps -- somewhat oddly called "nose flaps" -- to reduce takeoff distance. The tail was of swept tee configuration.

The Victor featured tricycle landing gear. The nose gear had twin wheels and retracted backward; each main gear unit consisted of eight-wheel bogies, with two rows of four tires, and retracted into the wings. Large hydraulic airbrakes were fitted to each side of the tailcone, and the tailcone contained a drag chute. B.1s were initially painted in a tidy overall "anti-flash white" to reflect the heat of a nuclear blast.

Handley Page Victor B.1/B.1A

The B.1 was fitted with four Armstrong-Siddeley Sapphire 7 202/207 turbojet engines with 49.0 kN (4,990 kgp / 11,000 lbf) thrust each. The engines were buried in the wingroots, a configuration that improved aerodynamics but made service access somewhat troublesome. In principle, a liquid-fuel de Havilland Spectre rocket pod could be attached under each wing between the engines to provide takeoff boost, but though the Spectre was trialed, it was never used in service.

The Victor carried a crew of five, including a pilot, copilot, two navigators, and an electronics systems officer, all in a spacious cockpit. Ejection seats were only provided for the pilot and copilot, on the basis that they would generally stay with the aircraft until the rest of the crew got out. There had been thought of building the entire crew compartment as an escape module, but the Air Ministry judged this measure too tricky and expensive.

The nose featured a large dielectric panel for H2S Mark IX navigation / targeting radar. The Victor could carry a single thermonuclear bomb, generally a British Blue Danube munition, later the Yellow Sun munition -- though it also carried American fusion weapons under a "dual command" arrangement. For conventional carpet bombing, the Victor B.1 could carry up to 35 450 kilogram (1,000 pound) bombs in its internal bombbay. The bombbay could also carry a long-range ferry tank as a alternate load.

Some sources state that the Victor had a heavier bombload than the much bigger Boeing B-52, but that was only true if the B-52's external bombload capability was ignored, and the B-52 also had a much longer unrefueled range. Sources also claim that the Victor could carry two of the World War II 5,440 kilogram (12,000 pound) Tallboy deep penetration bombs, or one of the Tallboy's "big brother", the 9,070 kilogram (20,000 pound) Grand Slam bomb. However, it is unclear if the Tallboy and Grand Slam were ever qualified on the Victor, and very uncertain that they were ever service weapons for the aircraft.

The production B.1 visibly differed from the two prototypes in a number of respects. The prototypes had proven uncomfortably tail-heavy, and so the forward fuselage was stretched by 1.07 meters (42 inches) and the height of the tailfin was cut to fix the problem. In addition, the crew door was moved to allow the crew to bail out without being sucked into the engines; cabin glazing was increased and rearranged; the tailfin fillet was eliminated and the tail tee-joint bullet fairing was modified; and the top of the outer wing was fitted with a set of small "vortex generator" airfoils to ensure proper low-speed airflow. The prototypes had two leading-edge flaps on each wing, but the production machines had only one.

The prototypes had also proven very responsive to control inputs -- too much so, in fact, making them "touchy", and as a result the production machines had "heavier" controls. The cockpit dashboard layout was also rearranged after initial trials, much to the frustration of Handley Page engineers; they had reviewed the matter with the Air Ministry in the design phase, but when it came time to actually fly the machine, the layout was judged "unacceptable".

* A total of 50 B.1s was built, with the last delivered in February 1961, and the B.1 also equipped RAF Numbers 15, 55, and 57 Squadrons. Three of the B.1s were fitted with Yellow Aster radar, a modification of the H2S Mark IX with a recording function, and attached to Number 543 Squadron for radar reconnaissance operations. Pictures survive of a B.1 fitted with large underwing antenna booms for the "Red Neck" side-looking radar system for radar reconnaissance, but the Victor never carried the Red Neck in service.

By the time the Victor was in full service, adversary fighters and other defenses were well able to reach or exceed the its speed and altitude. To improve the survivability of the type, 24 were modified to the "Victor B.1A" standard, being fitted with the Red Steer tail-warning radar; Blue Saga radar warning receiver (RWR); Green Palm voice communications jammer; Blue Diver & Red Shrimp radar jammers; and chaff dispensers.

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[3] VICTOR B.2 & SR.2

* Handley Page felt they could do better with the Victor, and in 1955 began work on the definitive "Victor B.2". A Victor B.1 was modified as the prototype, performing its initial flight on 20 February 1959. Unfortunately, this machine splashed into the Irish Sea in August 1959 during trials, the crew being lost. The program went ahead despite the mishap; the B.2 initially went into service with RAF Number 139 Squadron in February 1962. The B.2 also equipped RAF Number 100 Squadron.

The Victor B.2 featured:

Although some photos of early production Victor B.2s show them to have an externally "clean" configuration, they soon acquired a good deal of clutter in the form of a midair refueling probe, sticking out from the top of the cockpit; underwing tanks; a "hump" in front of the tailfin with jamming gear, featuring two pop-up "elephant ear" air intakes in front of it; and a countermeasures system in the tailcone, the cone being ringed with small antenna fairings. Apparently B.1s in service were also fitted with the flight refueling probe -- though only one carried the underwing tanks, as a trials fit.

Since the introduction of Soviet surface-to-air missiles (SAMs) had rendered high-altitude tactics obsolete, Victor B.2 flight operations were refocused on low-level tactics, the bombers being updated with low-altitude navigation radar and rolling map displays. Anti-flash white colors gave way to a disruptive camouflage scheme, with the first camouflaged B.2s going into service in early 1964.


   HANDLEY-PAGE VICTOR B.2:
   _____________________   _________________   _______________________
 
   spec                    metric              english
   _____________________   _________________   _______________________

   wingspan                36.48 meters        120 feet
   wing area               241.3 sq_meters     2,597 sq_feet
   length                  35.03 meters        114 feet 11 inches
   height                  8.57 meters         28 feet 1 inch

   empty weight            41,275 kilograms    91,000 pounds
   MTO weight              97,980 kilograms    216,000 pounds

   maximum speed           1,030 KPH           640 MPH / 555 KT
   service ceiling         16,000 meters       52,500 feet
   combat radius           3,700 kilometers    2,300 MI / 2,4000 NMI
   _____________________   _________________   _______________________

A total of 34 B.2s was built up to April 1963, with 21 of these quickly modified to the "Victor B.2R" specification, featuring:

The Victor was also to carry the US-built "Skybolt" air-launched ballistic missile, with the "HP.114" Victor launch platform featuring modified "gull" wings to carry two Skybolts under each wing, for a total of four. The Air Ministry felt Skybolt would give more bang for the money and decided to reduce the Victor production buy accordingly, but the Americans canceled the program in 1963, on the basis that other nuclear assets were more cost-effective. The British government had not been briefed on the cancellation, and there was considerable distress over the matter.

The Americans were apologetic over the matter and offered a number of proposals to reduce the impact of the decision on Britain's defense, one of them being to hand the Skybolt program over to the UK -- after a series of failures, test flights had been finally going well at the time it was axed. However, the British government reasonably much preferred the offer of adopting the Polaris submarine-launched missile system, and Skybolt stayed dead. Polaris was to be the future of Britain's nuclear deterrence, and until Polaris came online, existing tools would just have to make do. The Victor had to struggle on with the increasingly obsolescent Blue Steel.

Handley Page Victor B.2 with Blue Steel missile

The Victor never fired a shot in anger. In 1963, Victors were redeployed to Singapore in response to Indonesian hostility to Malaysia. Although there were some small border clashes during the confrontation, that was about as far as the conflict went, and the Victors never did perform any bombing attacks.

* In the early 1960s, the Vickers Valiant was the RAF's platform for the strategic reconnaissance role, but the Valiant fleet was permanently grounded in 1964 due to structural fatigue problems. There had already been plans to modify some of the Victor B.2s to the "Victor B(SR).2" strategic reconnaissance configuration, referred to in some sources simply as the "Victor SR.2". The program was accelerated to make up for the loss of the reconnaissance Valiants.

The first Victor B(SR).2 was flown on 23 February 1965. It featured the Yellow Aster radar, up to 15 film cameras in various arrangements in the bombbay, and carriage of photoflash flares; on occasion it also carried fallout-samping gear, fitted to the front of the wing tanks. A total of eight B.2s was converted to the B(SR).2 standard, with another B.2 converted to a partial reconnaissance standard while retaining Blue Steel capability. These machines were operated by RAF Number 543 Squadron, which received its first B(SR).2 in May 1965, with a focus on maritime reconnaissance. The B(SR).2 was a highly capable system, with a single machine capable of mapping the entire Mediterranean in one sortie.

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[4] VICTOR TANKERS

* With the introduction of the Victor B.2, the Victor B.1/1A was judged obsolescent for the bombing role. A B.1 was converted to a tanker configuration in 1964 to evaluate the usefulness of the type for midair refueling; while the evaluation was being conducted, the issue of converting the Victor to tanker operations suddenly became urgent. The Vickers Valiant was being used as a tanker up to that time, but the abrupt grounding of the Valiant fleet due to airframe weariness in that same year, 1964, meant the RAF suddenly needed new tankers right away and couldn't wait for the trials program to be completed.

Six B.1As were hastily fitted with a Flight Refueling FR.20B "hose and drogue unit (HDU)" under each wing to provide a two-point refueling capability. In principle, these machines were still capable of performing strike missions. They were originally designated "Victor B(K).1A", but redesignated as "Victor B.1A(K2P)" in 1968.

The initial tanker trials were completed and following conversions of the B.1/B.1A were more thorough, with these machines fitted with both the wing HDUs and an FR.17 centerline station, with a fuel tank in the bombbay. Eleven B.1s and fourteen B.1As were modified to this three-point configuration. These modified machines were originally designated "BK.1" and "BK.1A" respectively, changed to "K.1" and "K.1A" in 1968 since there was no thought of ever using them as bombers again. The first Victor tanker squadron, Number 57, became operational in February 1966, to be followed by Number 55 and 214 Squadrons.

Incidentally, the centerline HDU had a much bigger flow rate than the wing HDUs. The three-point tankers couldn't actually refuel three aircraft at the same time -- they could refuel one from the centerline HDU or two from the wing HDUs, but it wasn't safe to try to refuel an aircraft from the centerline HDU and a wing HDU at the same time.

* The Victor had not been designed for the low-level operational role, and by 1968 it was apparent that the B.2s would have to be retired from such duty, leaving the Avro Vulcan with its big robust delta wing to carry on in that function. The decision was made to refit the B.2s to a three-point tanker configuration. Handley Page had conducted technical studies on the matter from 1967, but the company went under in 1969, with the contract for the upgrades awarded to Hawker Siddeley in 1970. Hawker Siddeley completed the upgrade program, with some difficulty since the company had little expertise with the Victor, and had to start from scratch.

Handley Page Victor K.2

24 B.2s were upgraded to "Victor K.2" spec, with the first flying on 1 March 1972. All the bombing gear was removed, while the wing was strengthened and 46 centimeters (18 inches) were clipped off each wingtip to reduce flight stress -- altitude performance no longer being needed. The undernose glazing was finally eliminated. The K.2 could carry 44,700 kilograms (98,500 pounds) of fuel.

Number 543 Squadron was looted for B.2s to make the K.2s; as a result the squadron was disbanded in May 1974. The first Victor K.2s went into service with RAF Number 57 Squadron in July 1975, followed by service with RAF Number 55 Squadron beginning in April 1976. With the improved K.2s in service, Number 214 Squadron, which had been operating the old K.1s, was disbanded. The B(SR).2 reconnaissance machines had already been retired by this time, with the last withdrawn from service in 1975 for conversion to K.2s. They were replaced by reconnaissance-configured Avro Vulcan B.2s.

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[5] VICTOR IN ACTION

* Although the Victor never fired a shot in anger, it did see action in the tanker role. In 1982 Argentina seized the Falkland Islands in the South Atlantic, and as part of the operation to retake them, codenamed CORPORATE, the RAF was to conduct raids with Avro Vulcan bombers. The nearest RAF base was on lonely Ascension Island in the central Atlantic, so the Victor tanker was necessarily a critical factor in supporting bombing operations from the UK.

Even before the start of offensive operations, the Victor was performing radar reconnaissance over the South Atlantic, with four Victor tankers hastily modified for reconnaissance by tweaking their radars and installing provisions for cameras. From 20 April, Victors flew from Ascension to conduct radar sweeps of the ocean, in particular reporting on shipping and ice conditions for the assault fleet then on its way to the region. The reconnaissance missions were supported by Victors operating as tankers.

By the end of April, 14 Victors were operating out of Ascension to support strikes by Vulcans, the operation being codenamed BLACK BUCK. Each Vulcan attack involved a single bomber, supported by a number of Victors. The first BLACK BUCK strike was on 1 May, with a Vulcan bombing the runway at Port Stanley in the Falklands with high explosive (HE) bombs. It was the longest-ranging bomb raid that had ever been flown to that time; it was not only effective in denying local air support to the Argentine Falklands garrison, but also served notice to the Argentine government that the RAF could bomb Buenos Aires or other mainland targets, if so desired.

A second raid with HE bombs was flown on 3 May. Vulcans were then fitted with Shrike anti-radar missiles provided by the US, with a flight on 28 May being scrubbed inflight due to a technical problem with a Victor, but similar missions were flown on 29 May and 2 June, with Argentine radar installations successfully targeted and disabled. The fifth and last BLACK BUCK flight, carrying HE bombs fuzed for airburst to attack Argentine troops, was on 11 June, with the Argentine garrison finally throwing in the towel on 15 June.

* The Falklands campaign involved 600 Victor sorties and badly cut into the tanker fleet's airframe life, but 15 Victors remained in service long enough for one more campaign. The second set of combat operations of the Victor took place in the Gulf War. Following Saddam Hussein's invasion of Kuwait, an American-led Coalition assembled overwhelming force to throw him out. The RAF was a significant contributor to the effort, the British component being named Operation GRANBY, and eight Victors provided tanker support. The Victors flew 229 sorties, providing refueling services for US Navy aircraft along with the RAF fleet. Victors also provided tanker support for air patrols over Iraq into 1993.

Handley Page Victor K.2 tanker

However, that was the swan song of the Victor, since the Vickers VC.10 was gradually replacing it for tanker duties. The last Victor unit, Number 55 Squadron, was disbanded in October 1993, dissolving the very last remnant of the "V-force". At least five Victors survived, all remaining on display in the UK, but none are flying any more. One held in private hands could probably take to the air, but the civil aviation authority won't allow it, so the owner satisfies himself with high-speed taxi runs.

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[6] SUMMARY, COMMENTS, SOURCES, & REVISION HISTORY

* The following table gives a Victor variant and production summary:


  variant   built  updated   notes
  ___________________________________________________________________

  HP.80         2            Initial prototype.

  B.1          50            Initial bomber variant.
  B.1A          -       24   B.1 with improved ECM.
  B.1A(K2P)     -        6   B.1A quick bomber / tanker conversions.
  K.1           -       11   B.1 tanker conversion.
  K.1A          -       14   B.1A tanker conversion.

  B.2          34        -   Improved bomber, new engines, wider span.
  B.2R          -       21   B.2 with Blue Steel, uprated engines.
  B(SR).2       -        9   B.2 strategic reconnaissance configuration.
  K.2           -       24   B.2 tanker conversion.
  ___________________________________________________________________

  total        86
  ___________________________________________________________________

As with any successful aircraft, there were a number of unbuilt variants of the Victor. There was talk of a commercial airliner / transport derivative, with the same flight surfaces but a different fuselage, variously designated the "HP.97" and "HP.111". Handley Page also considered a supersonic Victor, with a redesigned forward fuselage, an "area-ruled" rear fuselage, a shorter wing, and new engines; as well as a design for a low-level bomber, with short wings, but it had little in common with the Victor except for the cockpit.

supersonic Victor

* As concerns copyrights and permissions for this document, all illustrations and images credited to me are public domain. I reserve all rights to my writings. However, if anyone does want to make use of my writings, just contact me, and we can chat about it. I'm lenient in giving permissions, usually on the basis of being properly credited.

* Sources include:

* Revision history:

   v1.0.0 / 01 may 05 
   v1.0.1 / 01 apr 07 / Review & polish.
   v1.1.0 / 01 apr 09 / General update.
   v1.1.1 / 01 apr 11 / Review & polish.
   v1.1.2 / 01 jan 13 / Review & polish.
   v1.1.3 / 01 jul 14 / Review & polish.
   v1.1.4 / 01 jun 16 / Review & polish.
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