Tupolev ANT-41

Source: Wikipedia, the free encyclopedia.
ANT-41
Role
Torpedo-bomber
National origin Soviet Union
Manufacturer Tupolev
Designer
Vladimir Myasishchev
First flight 2 June 1936
Number built 1

The Tupolev ANT-41 was a prototype Soviet twin-engined torpedo-bomber of the 1930s. A single prototype was built, which was destroyed in a crash. No production followed, with the Ilyushin DB-3 serving as a torpedo bomber instead.

Design and development

In March 1934, the

Vladimir Myasishchev.[1][4]

The ANT-41 was of similar layout to the contemporary

Alexander Arkhangelsky) at the Tupolev OKB, but was larger and more powerful. Like the SB, it was a mid-winged cantilever monoplane of all-metal stressed skin construction. It was powered by two Mikulin AM-34 liquid-cooled V12 engines in close-fitting cowlings driving 3-bladed propellers and cooled by radiators mounted inside the wings inboard of the engines, which were fed by narrow ducts on the leading edge of the wing.[5][6] A long (6.5 m (21 ft 4 in)) weapons bay under the fuselage could hold two 880 kilograms (1,940 lb) torpedoes, or a single 1,700 kilograms (3,700 lb) torpedo or an equivalent weight in bombs. The undercarriage of the landplane version was a retractable tailwheel undercarriage, based on that of the SB but strengthened to deal with the ANT-41's greater weight.[1][6]

History

The first prototype ANT-41, a landplane, made its maiden flight from Khodynka Aerodrome, Moscow on 2 June 1936, with severe tail flutter encountered.[4][6][nb 2] It was destroyed in a crash during the 14th test flight on 3 July 1936, with the test crew escaping by parachute. The accident was caused by flutter causing wing failure, which was traced to inadequate aileron design.[5][8] Later that year, the Ilyushin DB-3 was chosen to meet Soviet Naval Aviation's requirements for a torpedo bomber, and the ANT-41 was cancelled, with the second prototype unbuilt.[1]

Specifications

Data from Tupolev: The Man and His Aircraft[9]

General characteristics

  • Crew: 4
  • Length: 15.54 m (51 ft 0 in)
  • Wingspan: 25.73 m (84 ft 5 in)
  • Height: 3.86 m (12 ft 8 in)
  • Wing area: 88.94 m2 (957.3 sq ft)
  • Empty weight: 5,846 kg (12,888 lb)
  • Gross weight: 8,925 kg (19,676 lb)
  • Powerplant: 2 ×
    V-12 engines, 951 kW (1,275 hp) each [1]

Performance

  • Maximum speed: 435 km/h (270 mph, 235 kn)
  • Range: 4,200 km (2,600 mi, 2,300 nmi)
  • Service ceiling: 9,500 m (31,200 ft)

Armament

Notes

  1. ^ The Tupolev ANT-7 served in similar roles, but by 1934 was becoming obsolete.[2][3]
  2. ^ Similar tail flutter had been encountered during prototype testing of the SB,[4] and had caused the prototype Tupolev DB-2 long-range bomber to crash the previous year.[7]

Citations

  1. ^ a b c d e f g Gordon and Rigmant 2005, p. 74.
  2. ^ Gunston 1995, pp. 388–389.
  3. ^ Duffy and Kandalov 1996, p. 48.
  4. ^ a b c Duffy and Kandalov 1996, p. 84.
  5. ^ a b Gunston 1995, p. 407.
  6. ^ a b c Gunston Tupolev Aircraft since 1922 1995, p. 97.
  7. ^ Duffy and Kandalov 1995, p. 78.
  8. ^ Gunston Tupolev Aircraft since 1922 1995, p.98.
  9. ^ Duffy and Kandalov 1996, p. 209

References

  • Duffy, Paul and Andrei Kandalov. Tupolev: The Man and His Aircraft. Shrewsbury, UK: Airlife, 1996. .
  • Gordon, Yefim and Vladimir Rigmant. OKB Tupolev: A History of the Design Bureau and its Aircraft. Hinckley, UK: Midland Publishing, 2005. .
  • .
  • Gunston, Bill. Tupolev Aircraft since 1922. Annapolis, Maryland, USA: Naval Institute Press, 1995, .

External links