Neha Patil (Editor)

Yakovlev UT 2

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Top speed
  
210 km/h

Length
  
7.15 m

Manufacturer
  
Yakovlev

Wingspan
  
10 m

First flight
  
1937

Yakovlev UT-2 UT2 UT2M series planes by ASYakovlev

Designer
  
Alexander Sergeyevich Yakovlev

The Yakovlev UT-2 (Russian: Яковлев УТ-2; NATO reporting name "Mink") was a single-engine tandem two-seat low-wing monoplane that was the standard Soviet trainer during the Great Patriotic War. It was used by the Soviet Air Force from 1937 until replaced by the Yakovlev Yak-18 during the 1950s.

Contents

Yakovlev UT-2 WINGS PALETTE Yakovlev UT1UT2 Mink Hungary

Development

Yakovlev UT-2 Yakovlev UT2 Photo and video The history and characteristics

The preceding U-2 (Po-2) biplane was no longer a suitable trainer for the faster modern aircraft entering service, and to fill the role, the UT-2 was designed as a trainer.

Yakovlev UT-2 httpsuploadwikimediaorgwikipediacommonsthu

The new aircraft was designed by Alexander Sergeevich Yakovlev's team at OKB-115. Originally designated AIR-10, it was based upon the AIR-9, but it was simpler, with tandem open cockpits, also omitting slats and flaps. It first flew on 11 July 1935. The AIR-10 won the competition in 1935 and, after minor changes, was accepted as the standard Soviet Air Force trainer. With the disgrace of Alexey Ivanovich Rykov under whom Yakovlev had been working, the initials AIR were replaced with Ya making what would have been the AIR-20 the Ya-20 (Я-20).

Yakovlev UT-2 UT2

The wood-and-metal mixed construction of the AIR-10 was simplified to use only wood to facilitate production, and the AIR-10s 120 hp Renault inline engine was replaced with the 112 kW (150 hp) Shvetsov M-11E radial on the prototype, and the 82 kW (110 hp) M-11Gs in early production aircraft. Serial production started in September 1937. The Soviet VVS (Air Force) assigned the aircraft the designation UT-2 (uchebno-trenirovochnyi {учебно-тренировочный}, trainer).

Yakovlev UT-2 Yakovlev AIR20 UT2 sport training

The UT-2 was not easy to fly and easily entered into spins. The UT-2 model 1940 featured a lengthened forward fuselage, and a change to the 93 kW (125 hp) M-11D radial to attempt to rectify the problem. Despite improvements, the handling and flight characteristics remained challenging.

To further improve handling and stability, the new UT-2M (modernized) variant was developed in 1941 and it replaced the original UT-2 in production. The wing planform was redesigned, with a swept leading edge and a straight trailing edge, and the vertical stabilizer was enlarged.

7,243 UT-2 of all types were produced in five factories between 1937 and 1946. In the 1950s, the UT-2 was replaced by the Yak-18 primary trainer and the Yak-11 advanced trainer.

Before and after World War II the UT-2 was used by civilian organizations, and after the war, UT-2s were also operated by the Polish and Hungarian Air Forces.

Variants

AIR-10
precursor
AIR-11
three-seat prototype
Ya-20
prototype
UT-2
initial production variant
UT-2 (1940 standard)
improved spin characteristics.
UT-2 (1944 standard)
UT-2L
UT-2 with MV-4
inline engine for tests.
UT-2L
improved 1940 standard with canopy and engine cowling, fuselage similar to early Yak-18 but had fixed undercarriage.
UT-2M
production from 1941, new wings and empennage
UT-2MV
interim light bomber
UT-2N (SEN)
air cushion landing gear testbed
UT-2V
bomber trainer
VT-2
floatplane variant of basic UT-2
Yak-5
single-seat fighter-trainer development of UT-2L

Operators

 France
  • Normandie-Niemen unit
  •  Hungary
  • Hungarian Air Force
  •  Poland
  • Air Force of the Polish Army
  • Polish Navy
  •  Mongolia
  • Mongolian People's Air Force
  •  Romania
  • Romanian Air Force
  •  Soviet Union
  • Soviet Air Force
  •  Yugoslavia
  • SFR Yugoslav Air Force
  • 1st Training Aviation Regiment (1945-1948)
  • 104th Training Aviation Regiment (1948-1956)
  • Liaison Squadron of 5th Military district (1952-1956)
  • Liaison Squadron of 3rd Aviation Corps (1950-1956)
  • Survivors

    The Central Air Force Museum at Monino has an example on display, as does the Technical Museum of Vadim Zadorogny in Arkhangelsk.

    Specifications (UT-2, 1940 standard)

    Data from Gordon 2005, and Gunston 1995

    General characteristics

  • Crew: two
  • Length: 7.15 m (23 ft 5-1/2 in)
  • Wingspan: 10.2 m (33 ft 5-1/2 in)
  • Height: 2.99 m (9 ft 10 (tail up) in)
  • Wing area: 17.12 m2 (184.3 ft2)
  • Wing profile: Göttingen 387
  • Empty weight: 628 kg (1,385 lb)
  • Gross weight: 940 kg (2,073 lb)
  • Powerplant: 1 × Shvetsov M-11D 5 cylinder air-cooled Radial engine, 93.2 kW (125 hp)
  • Performance

  • Maximum speed: 210 km/h (131 mph)
  • Cruising speed: 99 km/h (60 mph)
  • Range: 1,130 km (702 miles)
  • Service ceiling: 5,000 m (16,400 ft)
  • Rate of climb: 3.3 m/s (649 ft/min)
  • Armament

  • None
  • References

    Yakovlev UT-2 Wikipedia