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Tupolev Tu 28

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Top speed
  
1,920 km/h

Wingspan
  
18 m

Weight
  
24,500 kg

First flight
  
1959

Range
  
2,565 km

Length
  
30 m

Engine type
  
Tupolev Tu-28 Tupolew Tupolev Tu28 Tu128 Specifications Technical Data

The Tupolev Tu-28 (NATO reporting name Fiddler) was a long-range interceptor aircraft introduced by the Soviet Union in the 1960s. The official designation was Tu-128, but this designation was less commonly used in the West. It was the largest and heaviest fighter ever in service.

Contents

Tupolev Tu-28 Tupolev Tu28 128UT The Tupolev Tu28 NATO reporting na Flickr

Background

Tupolev Tu-28 Tupolev Tu28 Tu128 interceptor

In the 1950s, the Soviet Union sought the means to defend against the nuclear-armed American bombers possibly penetrating its borders (especially its long and vulnerable northern border). Contemporary interceptors, even the Yakovlev Yak-28P, were able to cover only a radius of a few hundred kilometers; the newly developed surface-to-air missiles had even shorter range. Considering both, the sheer numbers required to defend a 5,000 km air front were economically impossible to maintain. This left the Soviet Union able to provide a modern air defense only for selected valuable areas. The PVO decided to cover the entire territory, but with a more loose defense. In 1955 it placed a requirement for a large area-defense interceptor, that would achieve it with sparse airbases. The PVO requirement called for a supersonic aircraft with enormous fuel tanks for both a good patrol time and a long range, a capable radar, and the most powerful air-to-air missiles possible. The first attempt, although an unsuccessful one, was a 30-tonne Lavochkin La-250 prototype, the last of the Lavochkin design bureau's aircraft.

Design and development

Tupolev Tu-28 httpsuploadwikimediaorgwikipediacommonsthu

Iosif Nezval of Tupolev Design Bureau led development of the new interceptor aircraft. The work began in 1958, based on an existing single prototype of the unsuccessful Tu-98 supersonic bomber. The military designation of the interceptor was at first Tu-28, but it had been changed in 1963 to Tu-128, identical to the designation used by the OKB.

Tupolev Tu-28 Tupolev Tu28 Wikipedia

The Tu-128 had a broad, low/mid-mounted swept wing carrying the main landing gear in wing-mounted pods, and slab tailplanes. Two Lyulka AL-7F-2 turbojet engines were mounted in the fuselage. The two-man crew of pilot and navigator were seated in tandem.

Tupolev Tu-28 WINGS PALETTE Tupolev Tu28Tu128 Fiddler USSRRussia

The Tu-128, with its maximum weight of 43 tonnes, was the heaviest fighter to enter service. It was a bomber interceptor, and with high wing loading, unsophisticated but reliable avionics and poor visibility, it was not an agile aircraft. It was intended to only combat NATO bombers like the B-52, not engage in dogfights with smaller aircraft.

Tupolev Tu-28 Tupolev Tu28 Tu128 interceptor

The interceptor made its initial public appearance on the 1961 Tushino air parade. Western experts, unaware that the bulge on the belly carried testing instruments, mistook it for a large ventral radar for a mixed interceptor/AWACS role. The production version lacked the bulge and had a large nose radome housing a radar, known as RP-S Smerch, with a detection range of about 50 km (31 mi) and a lock-on range of about 40 km (25 mi).

Tupolev Tu-28 WINGS PALETTE Tupolev Tu28Tu128 Fiddler USSRRussia

Armament of the Tu-128 was four Bisnovat R-4 air-to-air missiles (known as K-80 during development; NATO reporting name AA-5 'Ash'). Usually two of them were R-4R with semi-active radar homing and two were R-4T infrared-homing missile, with the former on the outer pylons and the latter on the inner underwing pylons. There was no internal weapons bay.

Production of the Tu-128 ended in 1970 with total 198 aircraft having been built.

Tupolev Tu-28 Tupolev Tu28 Tu128 Fiddler LongRange Interceptor Aircraft

Development of various projects designated Tu-28A, Tu-28-80, Tu-28-100, Tu-138, and Tu-148 were proposed by the Tupolev Design Bureau but all were abandoned.

Operational history

The Tu-128's only publicly reported combat operation was the destruction of NATO reconnaissance balloons. The aircraft remained in service until 1990. Through the 1980s, units armed with the Tu-128 converted to the Mikoyan MiG-31.

Variants

Prototype of Tu-28 ('Fiddler-A')
Development test aircraft, one built. OKB designation was 128. In the West, Fiddler-A was used for all the aircraft with twin ventral fins — these included a prototype and a few of initial production (perhaps two planes).
Tu-128 (also known as Tu-28; 'Fiddler-B')
Main version, first deployed operationally in 1964 (or 1966 – sources differ). The military designation was at first Tu-28, but the existing aircraft were renamed in 1963. The full designation of entire weapon complex (aircraft, radar, missiles) was Tu-128S-4. In the Western sources, but not in Soviet, often the more precise designation of this version is mentioned as either Tu-28P or Tu-128P.
Tu-128UT (also known as Tu-28UT)
Training version with an additional cockpit forward of the normal one, in place of a radar. 10 built and 4 converted from standard interceptors.
Tu-128M
A 1979 modernization of almost all existing aircraft for better interception at a low altitude. Development originated in 1970. Engines and airframe was not altered. The full designation of entire weapon complex was Tu-128S-4M. It contained a new RP-SM Smerch-M radar, and new missile set: R-4RM plus R-4TM.

Abandoned

Tu-28A
New development, abandoned.
Tu-28-80
Development designation, abandoned.
Tu-28-100
Development designation, abandoned.
Tu-138
New development, abandoned.
Tu-148
New development, abandoned.

Operators

 Soviet Union
  • Soviet Air Defence Forces
  • Never exported.
  • Specifications (Tu-128)

    Data from references

    General characteristics

  • Crew: Two, pilot and radar operator
  • Length: 30.06 m (98.62 ft)
  • Wingspan: 17.53 m (57.51 ft)
  • Height: 7.15 m (23.46 ft)
  • Wing area: 96.94 m² (1,043.45 ft²)
  • Empty weight: 24,500 kg (54,013 lb)
  • Loaded weight: 40,000 kg (88,185 lb)
  • Max. takeoff weight: 43,000–43,700 kg (94,800–96,342 lb)
  • Maximum g-loading: 2.5 g
  • Maximum fuel load: est. 13,600 kg (30,000 lb)
  • Powerplant: 2 × Lyulka AL-7F-2 afterburning turbojet
  • Dry thrust: 72.8 kN (7,425 kgf; 16,370 lbf) each
  • Thrust with afterburner: 99.1 kN (10,100 kgf; 22,270 lbf) each
  • Performance

  • Maximum speed: when armed 1,665 km/h (1,035 mph; est. 1.5 Ma) when unarmed 1,920 km/h (1,193 mph)
  • Range: 2,565 km when armed (1,595 mi)
  • Endurance: above 3 hours
  • Service ceiling: 15,600 m when armed (51,184 ft)
  • Maximum ceiling: 20,000 m (65,617 ft)
  • Armament

  • Hardpoints: 4
  • Missiles: 4 × Bisnovat R-4 air-to-air missiles (usually 2 × radar-guided R-4R and 2 × infrared-homing R-4T); other armament or tanks not used
  • References

    Tupolev Tu-28 Wikipedia


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