Puneet Varma (Editor)

Tupolev Tu 2

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Top speed
  
521 km/h

Wingspan
  
19 m

Length
  
14 m

First flight
  
January 29, 1941

Range
  
2,020 km

Weight
  
7,601 kg

Engine type
  
Tupolev Tu-2 Tupolev Tu2 Bat Fast Bomber Multirole Aircraft

The Tupolev Tu-2 (development names ANT-58 and 103; NATO reporting name Bat) was a twin-engine Soviet high-speed daylight and frontline (SDB and FB) bomber aircraft of World War II vintage. The Tu-2 was tailored to meet a requirement for a high-speed bomber or dive-bomber, with a large internal bombload, and speed similar to that of a single-seat fighter. Designed to challenge the German Junkers Ju 88, the Tu-2 proved comparable, and was produced in torpedo, interceptor and reconnaissance versions. The Tu-2 was one of the outstanding combat aircraft of World War II and it played a key role in the Red Army's final offensives.

Contents

Tupolev Tu-2 The Fire Hedgehog VIDEO Gunscom

Design and development

Tupolev Tu-2 Tupolew Tupolev Tu2 Specifications Technical Data Description

In 1937, Andrei Tupolev, along with many Soviet designers at the time, was arrested on trumped-up charges of activities against the State. Despite the actions of the Soviet government, he was considered important to the war effort and following his imprisonment, he was placed in charge of a team that was to design military aircraft. Designed as Samolyot (Russian: "aircraft") 103, the Tu-2 was based on earlier ANT-58, ANT-59 and ANT-60 light bomber prototypes. Essentially an upscaled and more powerful ANT-60 powered by AM-37 engines, the first prototype was completed at Factory N156, and made its first test flight on 29 January 1941, piloted by Mikhail Nukhtinov. Mass production began in September 1941, at Omsk Aircraft Factory Number 166, with the first aircraft reaching combat units in March 1942. Modifications were made based on combat experience, and Plant Number 166 built a total of 80 aircraft. The AM-37 engine was abandoned to concentrate efforts on the AM-38F for the Il-2, which required Tupolev to redesign the aircraft for an available engine. Modifications of this bomber took ANT-58 through ANT-69 variants. A further 2527 aircraft were built at Kazan, with these modifications. Production ceased in 1951 after a total of some 3,000 aircraft were delivered to various Soviet Bloc air forces.

Operational history

Tupolev Tu-2 httpsuploadwikimediaorgwikipediacommonsthu

Built from 1941 to 1948, the Tu-2 was the USSR's second most important twin-engine bomber (the first being the Pe-2). The design brought Andrei Tupolev back into favour after a period of detention. Crews were universally happy with their Tupolevs. Pilots could maneuver the aircraft like a fighter, it could survive heavy damage, and it was fast. The Tu-2 remained in service in the USSR until 1950.

Tupolev Tu-2 Tupolev Tu2 Wikipedia

Some surplus Tu-2s were provided to the Chinese People's Liberation Army Air Force for use in the Chinese Civil War. Some Chinese Tu-2s were shot down by United Nations airmen during the Korean War. In the 1958–1962 'counter-riot actions' in the 1959 Tibetan uprising in Qinghai-Tibet Plateau covering Qinghai, Tibet, southern Gansu, and western Sichuan, Chinese PLAAF Tu-2s took on the roles of ground-attack, reconnaissance and liaison. The Chinese Tu-2s were retired at the end of the 1970s.

After World War II, the Tu-2 proved to be an ideal test aircraft for various powerplants, including the first generation of Soviet jet engines.

Variants

"Aircraft 103" (ANT-58)
The initial three-seat version. Top speed 635 km/h (395 mph) at 8,000 m (26,247 ft). Two 1,044 kW (1,400 hp) Mikulin AM-37 (water cooling), 1941.
"Aircraft 103U" (ANT-59)
Redesigned for four-seat crew (influenced by Junkers Ju-88). Top speed dropped to 610 km/h (379 mph). It used the same engines as the ANT-58.
"Aircraft 103V" (ANT-60)
As ANT-59 but powered by air-cooled Shvetsov ASh-82 engines after the AM-37 was cancelled.
"Aircraft 104"
Tu-2S modified for interceptor role.
ANT-62T
Torpedo bomber prototype developed from the Tu-2D.
ANT-63 (SDB)
High-speed day bomber prototype.
ANT-64
Long-range four-engine heavy bomber project developed from the Tu-2, cancelled in favor of Tu-4. Also known as Tu-10.
ANT-66
Airliner variant of ANT-64.
ANT-67
Five-seat long-range bomber similar to ANT-62 but powered by Charomskiy ACh-30BF diesel engines, 1946.
Tu-1 (ANT-63P)
Prototype three-seat night fighter version.
Tu-2
Two 1,081 kW (1,450 hp) Shvetsov ASh-82 (air cooling) with bigger drag, 1942.
Tu-2D (ANT-62)
Long-range version, it appeared in October 1944. It had an increased span and a crew of five aviators. Powered by two 1,380 kW (1,850 hp) Shvetsov ASh-82FN?, 1943?
Tu-2DB (ANT-65)
High-altitude reconnaissance bomber version developed from the Tu-2D, powered by two turbo-supercharged Mikulin AM-44TK engines.
Tu-2F
Photo-reconnaissance version.
Tu-2G
High-speed cargo transport version.
Tu-2K
Only two aircraft were built for testing ejection seats.
Tu-2LL
Tu-2's modified as testbeds.
Tu-2M (ANT-61M)
Powered by two 1,417 kW (1,900 hp) ASh-83 radial piston engines.
Tu-2N
Engine testbed, built to test the Rolls-Royce Nene turbojet engine.
Tu-2 Paravan
Two aircraft built to test barrage balloon cable cutters and deflectors.
Tu-2R
Reconnaissance version.
Tu-2RShR
Prototype, armed with 57 mm cannon in the forward fuselage.
Tu-2S (ANT-61)
Powered by two 1,380 kW (1,850 hp) Shvetsov ASh-82FN radial piston engines, 1943.
Tu-2S RLS PNB-4
secretive night-fighter prototype developed under leadership of the NKVD special section of V. Morgunov and P. Kuksenko. Equipped with the Soviet Gneiss 5 (Гнейс 5) radar. Armed with two NS-45 autocannons. Development presumed to have started in 1943. Precursor of the Tu-1.
Tu-2Sh
Experimental ground-attack versions. Two variants were tested in 1944: one with a 76mm (2.95 inches) centerline gun and another with a battery of 88 7.62mm (0.30 inches) PPSh-41 submachine guns fixed in the bomb bay, directed to fire ahead at a 30-degree angle. Another version under this designation was tested in 1946; this one had a frontal armament consisting of with two NS-37 and two NS-45 autocannons.
Tu-2T
Torpedo-bomber variant, was tested between February and March 1945, and issued to Soviet Naval Aviation units.
Tu-2U
Trainer version.
Tu-2/104
All-weather interceptor prototype.
Tu-6
Reconnaissance prototype, 1946.
Tu-8 (ANT-69)
Long-range bomber based on Tu-2D, 1947.
Tu-10 (ANT-68)
It was a high-altitude variant that saw limited service, 1943.
Tu-12
Medium-range jet bomber prototype, 1947.
UTB
bomber trainer with Shvetsov ASh-21 engines of 515 kW (690 hp) created by the Sukhoi OKB in 1946

Operators

World War II operators
 Soviet Union
  • Soviet Air Force
  • Postwar operators
     Bulgaria
  • Bulgarian Air Force
  •  China
  • People's Liberation Army Air Force Imported 33 UTB-2 and 29 T-2U trainers at the end of 1949. The last four UTB-2s retired in 1965. Imported 311 Tu-2s from the end of 1949 to 1952. The last 30 Tu-2s retired in 1982.
  •  Hungary
  • Hungarian Air Force
  •  Indonesia
  • Indonesian Air Force
  •  North Korea
  • North Korean Air Force
  •  Poland
  • Polish Air Force (eight aircraft in 1949-early 1960s)
  • Polish Navy
  •  Romania
  • Romanian Air Force (six delivered in 1950: two Tu-2s, two Tu-2 trainers and two Tu-6s)
  •  Soviet Union
  • Soviet Air Force
  • Aircraft on display

  • Bulgaria
  • Bulgarian Museum of Aviation – Tu-2T, tactical number 27
  • China
  • Military Museum of the Chinese People's Revolution, Beijing
  • Chinese Aviation Museum near Beijing
  • Poland
  • Polish Aviation Museum in Kraków – Tu-2S, used for testing ejection seats
  • Museum of the Polish Army in Warsaw – Tu-2S, used by 7th Independent Dive Bomber Regiment ("7 samodzielny pułk lotniczy bombowców nurkujących")
  • Russia
  • Central Air Force Museum in Monino near Moscow
  • USA
  • War Eagles Air Museum in Santa Teresa, New Mexico
  • Specifications (Tu-2)

    Data from

    General characteristics

  • Crew: four
  • Length: 13.80 m (45 ft 3 in)
  • Wingspan: 18.86 m (61 ft 10 in)
  • Height: 4.13 m (13 ft 7 in)
  • Empty weight: 7,601 kg (16,757 lb)
  • Loaded weight: 10,538 kg (23,232 lb)
  • Max. takeoff weight: 11,768 kg (25,944 lb)
  • Powerplant: 2 × Shvetsov ASh-82 radial engine, 1,380 kW (1,850 hp) each
  • Performance

  • Maximum speed: 528 km/h (281 kn, 325 mph)
  • Range: 2,020 km (1,090 nmi, 1,260 mi)
  • Service ceiling: 9,000 m (29,528 ft)
  • Rate of climb: 8.2 m/s (1,610 ft/min)
  • Wing loading: 220 kg/m² (45 lb/ft²)
  • Power/mass: 260 W/kg (0.16 hp/lb)
  • Armament

  • Guns:
  • 2 × 20 mm (0.79 in) fixed forward-firing ShVAK cannon in the wings
  • 3 × 7.62 mm (0.30 in) rear-firing ShKAS machine guns (later replaced by 12.7 mm (0.50 in) Berezin UB machine guns) in the canopy, dorsal and ventral hatches.
  • Bombs: 1,500 kg (3,300 lb) internally and 2,270 kg (5,000 lb) externally
  • References

    Tupolev Tu-2 Wikipedia


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