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Tupolev Samolyot 135

Military Aircraft

The Tupolev Samolyot 135 was a designation used for two different strategic bomber projects in the Soviet Union in the late 1950s and early 1960s, neither of which progressed beyond the drawing board. The first, proposed in 1958, was a Tu-95 derivative carrying a long-range cruise missile, with an estimated range of about 4,000 km. Two years later the second was envisioned as a supersonic interdiction bomber available with a variety of engines, including a nuclear-powered version. It settled on a canard delta layout similar to the North American XB-70A Valkyrie, with paired Kuznetsov NK-6 turbofan nacelles under each wing and a single large fin, and armed mainly with missiles for maritime and logistics interdiction. Work was suspended when the Sukhoi T-4 became the favoured design and the cost proved high, though the experience helped later Tupolev bombers and the Tu-144, which carried the code name Tu-135P.

Facts
Engine Class
Turbofan 1
Status
Design only (never built) 1
Comparison
Body Style
Aircraft (no road body style) 1
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Aviation, Modes
Source Tupolev Samolyot 135 (Wikipedia)

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Source Tupolev Samolyot 135 (Wikipedia)
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Source Tupolev Samolyot 135 (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The Tupolev Samolyot 135 was a designation

Originated In

Also in Geography Atlas: where this subject originated.

Source Tupolev Samolyot 135 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
strategic bomber projects in the Soviet Union
Sources
1. Tupolev Samolyot 135 (Wikipedia)
  • Lead
    was a designation that was used for two different strategic bomber projects in the Soviet Union
  • Lead, status
    neither of which progressed beyond the drawing board
  • Design and development
    paired Kuznetsov NK-6 turbofan engine nacelles under each wing
  • Lead, manufacturer
    The Tupolev Samolyot 135 was a designation
  • Lead, country of origin
    strategic bomber projects in the Soviet Union
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