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Contents

   



(Top)
 


1 Development  



1.1  ANT-28  







2 Specifications (TB-6 estimated)  





3 References  














Tupolev TB-6






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TB-6/ANT-26/ANT-28
Role Bomber
National origin Soviet Union
Manufacturer Tupolev
Designer Andrei Tupolev, Vladimir Petlyakov
Primary user Red Air Force (intended)
Number built 0
Developed from ANT-16

Tupolev TB-6 (internal designation ANT-26; Russian: Туполев ТБ-6/АНТ-26) was a proposal by the Tupolev Design Bureau in the 1930s for a super-heavy bomber. Had it been built, it would have been the biggest-ever Soviet bomber and the largest aircraft by wingspan of its time, nine feet short of the 320 foot span of the Hughes H-4 Hercules, although the Scaled Composites Stratolaunch is now the biggest plane by wingspan.

Development

[edit]

While undertaking development of the Tupolev ANT-16 and ANT-20/PS-124, Tupolev began work in 1931 on an even larger bomber aircraft, powered by 12 engines and with a takeoff weight of 70,000 kg (150,000 lb). The resulting ANT-26 design was to have 12 Mikulin M-34FRN engines, eight on the leading edge of the wing and four in two tandem pairs above the wings. The tail empennage would have had three vertical stabilizers on the tailplane, the center vertical stabilizer taller than the others. An alternative TB-6 design featured a bomber aircraft with six Mikulin M-44 engines and a single rudder.[1]

Given the sheer size of the TB-6, Tupolev decided to build a sub-scale aircraft to test the flight behavior of the TB-6. The subscale model flew in 1935, piloted by B.N. Koodrin. However, by the mid-1930s the trend in military aviation shifted towards smaller and faster aircraft and the TB-6 was cancelled, by which time the airframe was 75 percent complete and the entire aircraft 16 percent complete.[2]

ANT-28

[edit]
Desktop model of Tupolev ANT-28

In parallel with design of the ANT-26, the Tupolev Design bureau envisaged a vastly scaled-up ANT-20 with the same dimensions as the ANT-26 under the internal designation ANT-28 It was intended as an airliner and cargo plane with a maximum payload of 15,000 kg and a range of 1,500 km, and the arrangement of the engines was the same as for the TB-6. Like the TB-6, the ANT-28 never progressed past the drawing board.[3]

Specifications (TB-6 estimated)

[edit]

Data from Istoriia konstruktskii samoletov v SSSR do 1938,[2] The Osprey Encyclopaedia of Russian Aircraft 1875–1995.[4]

General characteristics

Performance

Armament

References

[edit]
  1. ^ Gordon, Yefim; Rigamant, Vladimir (2005). OKB Tupolev: A History of the Design Bureau and its Aircraft. Hinckley, England: Midland Publishing.
  • ^ a b Shavrov V.B. (1985). Istoriia konstruktskii samoletov v SSSR do 1938 g. (3 izd.) (in Russian). Mashinostroenie. ISBN 5-217-03112-3.
  • ^ "ANT-26 (TB-6) Heavy bomber (Project)".
  • ^ Gunston, Bill (1995). The Osprey Encyclopaedia of Russian Aircraft 1875–1995 (1st ed.). London: Osprey Publishing. ISBN 978-1-85532-405-3.
  • Duffy, Paul and Andrei Kankdalov. (1996) Tupolev The Man and His aircraft. Warrendale, PA: Society of Automotive Engineers.


    Retrieved from "https://en.wikipedia.org/w/index.php?title=Tupolev_TB-6&oldid=1090805195"

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    This page was last edited on 31 May 2022, at 13:19 (UTC).

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