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Tupolev ANT-21

From Wikipedia, the free encyclopedia
ANT-21 (MI-3)
RoleFighter
Type of aircraft
National originSoviet Union
ManufacturerTupolev
First flight1933
Number built2
Developed fromTupolev ANT-7

TheTupolev ANT-21 was aSoviet twin-engined four-seat heavyfighter, which also had the designationMI-3 (Mnogomestnyi Istrebitel – Multi-seat fighter). It was not accepted for production, only two prototypes being built.

Design and development

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In January 1932, theSoviet Air Forces ordered theTsAGI design bureau led byAndrei Tupolev to design a twin-engined multi-seat fighter to replace the KR-6 escort fighter version of theTupolev ANT-7 twin-engined multi-purpose aircraft. Tupolev assigned design of the new fighter to a team led byAlexander Arkhangelsky. This was Arkhangelsky's first project as chief designer. The resulting aircraft, the ANT-21, was like the ANT-7, amonoplane, with its corrugated all-metal wings based on those of the ANT-7, but having reduced span, and with the corrugations covered in fabric to reduce drag. The oval-section fuselage was a new design, being a partiallyflush riveted semi-monocoque structure made ofduralumin, a first for Tupolev aircraft, and it was fitted with a twin tail. It also had a retractabletailwheel undercarriage, novel for the time.[1][2][3]

The aircraft's pilot sat in an open cockpit above the leading edge of the wing. One gunner sat in the nose operating two machine guns, a second gunner sat in a dorsal position with two more machine guns, while another crewman operated a ventral gun, firing through a hatch. Two fixed machine guns could be operated by the pilot. TwoMikulin M-17 engines powered the ANT-21, as used by the ANT-7.[1][2]

The first prototype, officially designated MI-3 and nicknamedMitrich made its maiden flight in August 1933.[1][3] Initial testing was successful, the ANT-21 being popular with its test pilots, but when being dived at nearly 400 km/h (250 mph), severeflutter was encountered in the aircraft tail, with the starboard rudder breaking off and the aircraft making a heavy landing.[1][2]

As a result of this accident, Arkhangelsky redesigned the aircraft, retaining the wings, but providing a new fuselage and tail, with a single vertical fin. The crew were accommodated in enclosed cockpits, with the nose gunner operating a single 20mm cannon or a heavy machine gun and the ventral gun being omitted, while the dorsal gunner's armament and the fixed guns operated by the pilot were unchanged. The M-17 engines of the first prototype were replaced by more powerful and modernM-34Ns.[1] The new aircraft, the ANT-21bis or MI-3D (Doubler – understudy) was completed in April 1934. Despite the new tail, it suffered tail vibration at certain power settings which resulted in the addition of tail-bracing struts. It was officially tested during July–December 1934, but was not accepted for service by the Soviet Air Force, as it now wanted fighters armed with heavyrecoilless rifles, and interest switched to theTupolev ANT-29 derivative.[4]

Specifications (ANT-21D)

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Data from The Osprey Encyclopedia of Russian Aircraft 1975–1995[1]

General characteristics

  • Crew: three
  • Length: 11.57 m (38 ft 0 in)
  • Wingspan: 20.76 m (68 ft 1 in)
  • Wing area: 59.2 m2 (637 sq ft)
  • Empty weight: 4,058 kg (8,946 lb)
  • Gross weight: 5,463 kg (12,044 lb)
  • Powerplant: 2 ×M-34N liquid-cooledV12 engine, 610 kW (820 hp) each

Performance

  • Maximum speed: 350 km/h (220 mph, 190 kn) at 5,000 m (16,400 ft)
  • Service ceiling: 8,300 m (27,200 ft)

Armament

Notes

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  1. ^abcdefGunston 1995, pp. 396–397.
  2. ^abcKandalov and Duffy 1996, p. 64.
  3. ^abGreen and Swanborough 1994, p. 571.
  4. ^Green and Swanborough 1994, pp. 571–572.

References

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  • Duffy, Paul and Andrei Kandalov.Tupolev The Man and His Aircraft. Shrewsbury, UK:Airlife Publishing, 1996.ISBN 1-85310-728-X.
  • Green, William and Gordon Swanborough.The Complete Book of Fighters. New York, Smithmark, 1994.ISBN 0-8317-3939-8.
  • Gunston, Bill.The Osprey Encyclopedia of Russian Aircraft 1875–1995. London:Osprey, 1995.ISBN 1-85532-405-9.
Tupolev aircraft
Civilian
Military
Unmanned
Experimental
Proposed,
cancelled
Early period
Sovietfighter designations, 1923–1940
Fighters (I)
Two-seat fighter (DI)
Multi-seat fighter (MI)
Cannon fighter (IP)
Descriptors
1 Unknown/not assigned
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