Tupolev Samolyot 135
The Tupolev Samolyot 135 refers to two separate strategic bomber initiatives developed in the Soviet Union during the late 1950s and early 1960s, neither of which advanced beyond conceptual stages.
Design and development
The initial concept, introduced in 1958, involved a modification of the Tupolev Tu-95 to carry a long-range cruise missile. This missile was intended to be based on designs such as the Tsybin RS (S-30), Tupolev Samolyot 100, or Tupolev Samolyot 113. The combined system was projected to achieve an operational radius near 4,000 km (2,500 mi).[1][2]
By 1960, a second version of the '135' emerged, envisioned as a supersonic interdiction bomber powered by various engine configurations, including options for nuclear propulsion. The finalized design featured a canard delta wing layout reminiscent of the North American XB-70A Valkyrie, equipped with paired Kuznetsov NK-6 turbofan engines mounted in nacelles beneath each wing and a prominent single vertical stabilizer. The aircraft’s armament was planned to focus primarily on missile weaponry for both maritime strike missions and extended interdiction of enemy supply lines. Throughout its development, this design underwent multiple refinements and provided Tupolev with critical experience that contributed to the subsequent creation of the Tupolev Tu-22M and Tupolev Tu-160 bombers.[1][2]
Progress on the '135 program was ultimately halted in favor of the Sukhoi T-4 project during the early 1960s, influenced by the projected high costs associated with the '135'. Various versions were explored, including the 135K variant intended for maritime strike and interdiction roles; the '135P' proposed as a supersonic transport (SST); and a reconnaissance model equipped with cameras and electronic intelligence (ELINT) systems.[3][2]
Estimated Technical Details
References
External links
- "Tu-135". airwar.ru. Retrieved 2018-09-06.
- ""135" (Tu-135) supersonic strategic bomber". alternathistory.com. Retrieved 2018-09-06.