Глостер Джавелин: Британский перехватчик эпохи холодной войны

British interceptor aircraft

The Gloster Javelin is a twin engined all weather interceptor aircraft that served with Britain's Royal Air Force from the mid 1950s until the late 1960s. It was a T tailed delta wing aircraft designed for night and all weather operations and was the last aircraft design to bear the Gloster name. Introduced in 1956 after a lengthy development period, the aircraft received several upgrades during production to its engines, radar and weapons, including support for the De Havilland Firestreak air to air missile. The Javelin was succeeded in the interceptor role by the English Electric Lightning, a supersonic aircraft capable of flying at more than double the Javelin's top speed, which was introduced into the RAF only a few years later. The Javelin served for much of its life alongside the Lightning; the last Javelins were withdrawn from operational service in 1968 following the introduction of successively more capable versions of the Lightning.

In the aftermath of the Second World War, Britain identified a threat posed by the jet powered strategic bomber and atomic weaponry and thus placed a great emphasis on developing aerial supremacy through continuing to advance its fighter technology, even following the end of the conflict. Initial planning was based on the premise that another war was at least ten years away, and development was limited mostly to paper projects. Several events in the late 1940s led to this timeline being moved up. In 1947, the Air Ministry issued a requirement for a high performance night fighter under specification F.44/46. It called for a two seat design that would intercept enemy aircraft at heights of up to at least 40,000 feet. It would also have to reach a maximum speed of 525 kn (973 km/h, 605 mph) at this height, be able to perform rapid ascents and attain an altitude of 45,000 feet within ten minutes of engine ignition. Additional criteria given in the requirement included a minimum flight endurance of two hours, a takeoff distance of 1,500 yards, structural strength to support up to 4g manoeuvres at high speed and for the aircraft to incorporate airborne interception radar, multi channel VHF radio and various navigational aids. The aircraft would also be required to be economical to produce, at a rate of ten per month for an estimated total of 150 aircraft.

Gloster Aircraft developed and produced the only British jet aircraft to be operational during the war, the Gloster Meteor. Through the post war period, they produced a series of updated versions of the Meteor, including some with delta wing layouts for all or the outer portion of the wings. These were further developed by moving the engines to the fuselage and using a complete delta wing layout, leading to a second series of designs that continued in parallel. P.228, drawn up in 1946, was essentially a two seat Meteor with slightly swept wings. A similar design was also offered to the Royal Navy as the P.231. The later issued P.234 and P.238 of early 1947 had adopted many of the features that would be distinctive of the Javelin, including the large delta wing and tailplane, and were based on the Rolls Royce AJ65 engine (better known as Avon). The two differed primarily in role; P.234 was a single seat day fighter with a V tail, while P.238 was a two seat night fighter with a mid mounted delta tailplane. The Air Ministry released more detailed specifications on 17 Jun 1949, as F.4/48. Gloster responded with two further updated designs, P.300, which was essentially a quick update to the Meteor with two seats and newer Derwent engines, and the P.316/P.317, another update to the delta layout mounting the Sapphire engines. The P.316 and 317 differed primarily in role, 316 was a single seat design lacking radar and mounting up to four bombs in containers under the fuselage, while 317 was a two seat design with radar and some form of heavy armament to be determined. The RAF requirements were subject to some changes, mainly in regards to radar equipment and armaments; Gloster also initiated some changes as further research was conducted into the aerodynamic properties of the new swept and delta wings, as well as use of the new Armstrong Siddeley Sapphire turbojet engine.

On 13 April 1949, the Ministry of Supply issued instructions to two aircraft manufacturers, Gloster and de Havilland, to each construct four airworthy prototypes of their competing designs to meet the requirement, as well as one airframe each for structural testing. These prototype aircraft were the Gloster GA.5, designed by Richard Walker, and the de Havilland DH.110, the latter of which held the advantage of also being under consideration for the Royal Navy. Development was considerably delayed through political cost cutting measures, the number of prototypes being trimmed down to an unworkable level of two each before the decision was entirely reversed; this led to the unusual situation where the first production Javelin was completed before the prototype order being fulfilled. The first prototype was completed in 1951. An unusual feature of the prototypes was the opaque canopy over the rear cockpit. It had been believed that visibility outside the cockpit was unnecessary and a hindrance to the observer; the only external view available was through 2 small 'portholes'. Following a month of ground testing, on 26 November 1951, the first prototype conducted its first flight at Moreton Valence airfield. Bill Waterton, Gloster's Chief Test Pilot, would later describe the Javelin as being "as easy to fly as an Anson", although also expressing concern over its inadequate power controls. Disaster nearly struck during one test flight when aerodynamic flutter caused the elevators to detach in mid flight; despite the lack of control surfaces, Bill Waterton was able to land the aircraft using tailplane trimming and engine thrust for pitch control. He was awarded the George Medal for his actions to retrieve flight data from the burning aircraft. The second prototype (WD808) received a modified wing in 1953. After initial testing by Waterton, it was passed to another Gloster test pilot, Peter Lawrence for his opinion. On 11 June 1953, the aircraft crashed during testing. Lawrence had ejected from the aircraft, but too late (at about 400 feet (122 m)), and was killed. The Javelin had experienced a "deep stall"; the wing acting like an airbrake had killed forward motion and at the same time degraded the airflow over the elevators, leaving them useless. Without elevator control, Lawrence was unable to regain control and the aircraft dropped from the sky. The third prototype (WT827), and the first to be fitted with operational equipment including radar, first flew on 7 March 1953. The fourth prototype (WT830) was passed to the Aeroplane and Armament Experimental Establishment (A&AEE) for trials and the fifth prototype, WT836, made its first flight in July 1954. On 4 July 1954, a prototype Javelin accidentally achieved supersonic speed during a test flight, the pilot having been distracted by an oxygen supply failure.

The official production order for the Javelin was issued in mid 1953; as the Gloster Meteor was still being actively produced by Gloster, considerable elements of the Javelin were subcontracted out to other aviation companies owned by the Hawker Siddeley Group, such as Armstrong Whitworth. On 21 October 1954, a pilot attached to Gloster from RAE Farnborough was killed while flying Javelin XA546 having entered what appeared to be an intentional spin. was testing XA561 for the A&AEE when the aircraft entered a flat spin at 40,000 ft during manoeuvres testing the buffet boundary, which the anti spin parachute could not stop, and he chose to eject at 8,000 ft. Following this, a stall warning device was developed for the Javelin. By the end of 1956, the Javelin was up to a FAW 7 variant, which was the first to meet the specifications of the original Air Ministry requirement, and which was to become the definitive version of the aircraft (most of which were later altered to the FAW 9 standard). The Javelin was evolving so quickly that deliveries of the FAW 8 began before FAW 7 production had ended. As a result, the final 80 FAW 7 aircraft went straight from the factory into storage, eventually flying after being re manufactured as FAW 9s. A total of 427 Javelins were produced in all variants, plus seven prototypes. While there had been considerable interest from several NATO air forces, there were no export orders for the Javelin.

The Javelin was the RAF's first purpose built all weather interceptor aircraft. Aerodynamic features of the type included its adoption of the new delta wing and a large tailplane. Fuel and armaments were housed in the delta wing, and the engines and crew in the fuselage. The delta wing and tailplane combination had been deemed necessary by Gloster for effective manoeuvrability at high speed and for the aircraft to be controllable at low landing speeds. In one instance during testing, when both elevators had been torn off by elevator flutter, the Javelin remained controllable by using both the trimming capability of the large tailplane and thrust changes to control pitch. Changes from the prototypes included alterations to the rear fuselage and a central "pen nib" fairing extending beyond the engine nozzles, to eliminate buffeting of the rudder by the jet exhaust and increased sweepback of the wing's leading edge to improve high speed handling. The Javelin was reportedly easy to fly even on one engine. The flight controls were fully power assisted and production aircraft adopted a hydraulic 'feel' system for the pilot. The Javelin featured an infinitely variable airbrake; the airbrake proved to be extremely responsive and effective, allowing pilots to conduct rapid descents and heavy braking manoeuvres, enabling equally rapid landings to be performed. The turnaround time between sorties was significantly shorter than with the preceding Gloster Meteor, due to improved ground accessibility and engine ignition sequence. Unlike the Meteor, the Javelin was fitted with ejector seats, at the introduction to service of the type. No other operational fighter of the West even to the present day had a bigger wing, in terms of area, than the Javelin, and in the USSR, only the Tu 128 had a larger (about 10m2) wing. In spite of the aircraft's unorthodox aerodynamic features, the Javelin had a fairly conventional structure and materials, being mainly composed of an aluminium alloy, with some use of steel edging. The fuselage was composed of four sections, the nose (containing the radar radome), the front fuselage, centre fuselage and rear fuselage; the nose and rear fuselage were removable for servicing and easy replacement. The engines were on either side of the centre fuselage, the internal space in the centre containing the service bay that housed much of the aircraft's electrical, hydraulic, and avionics subsystems.

Several variants were proposed and investigated but not produced, including aerial reconnaissance versions, a fighter bomber version with underwing panniers for bombs, and a supersonic variant with area ruled fuselage, thinner wings, and a new tail. The "thin wing Javelin" would have been capable of about Mach 1.6, with a higher ceiling than contemporary US designs. Initial work started with fitting a thinner section wing to a Javelin fuselage but as the project developed the changes became so great that it would effectively have been a different aircraft albeit having an outward resemblance to the Javelin. The Gloster P.370 to F.153D for "Thin Wing Gloster All Weather Fighter, an update of the initial F.118 specification was ordered in 1954; a prototype XG336 along with two pre production aircraft. The final incarnation of the thin wing Gloster (P.376) just before cancellation was a large aircraft carrying two Red Dean all aspect missiles as a possible contender for Operational Requirement F.155. The aircraft, then under construction, and the missile were cancelled in 1957.