title: Tupolev Samolyot 135
text: # Tupolev Samolyot 135
  
  The Tupolev Samolyot 135 was a designation that was 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.
  
  ## Design and development
  
  The first, proposed in 1958, was for a Tupolev Tu-95 derivative carrying a long-range cruise-missile, to be based on the Tsybin RS (S-30), Tupolev Samolyot 100 or Tupolev Samolyot 113 missiles. The combination was estimated to have a total range of approximately 4,000 km (2,500 mi).
  
  Two years later the second iteration of '135' was envisioned as a supersonic interdiction bomber powered by a variety of engines in many configurations, including as a nuclear-powered bomber. The design settled to a canard delta, similar to the North American XB-70A Valkyrie, with paired Kuznetsov NK-6 turbofan engine nacelles under each wing and a large single fin. Weapons would largely have been missiles, as designed, for maritime interdiction as well as long-range interdiction of enemy logistics. The design was constantly evolving and gave Tupolev valuable experience which would assist in the later design of the Tupolev Tu-22M and Tupolev Tu-160 bombers.
  
  Further development of the '135 was suspended when the Sukhoi T-4 became the favoured outcome of the design efforts in the early 1960s,as well as high estimated cost of the '135'. Variants that were studied included: the 135K maritime strike / interdiction; '135P' supersonic transport (SST); a reconnaissance variant with cameras and ELINT equipment.
  
  ## Specifications (estimated)
  
  Data from , OKB Tupolev
  
  General characteristics
  
  * Crew: 4
  * Length: 50.7 m (166 ft 4 in)
  * Wingspan: 34.8 m (114 ft 2 in)
  * Height: 10.7 m (35 ft 1 in)
  * Wing area: 417 $m^2$ (4,490 sq ft)
  * Gross weight: 175,000 kg (385,809 lb)
  * Max takeoff weight: 205,000 kg (451,948 lb)
  * Powerplant: 4 × DTRD NC-6 turbofan engines, 105 kN (23,500 lbf) with afterburner
  
  Performance
  
  * Maximum speed: 3,000 km/h (1,900 mph, 1,600 kn)
  * Cruise speed: 2,650 km/h (1,650 mph, 1,430 kn)
  * Range: 7,800 km (4,800 mi, 4,200 nmi) to 8,000 km (5,000 mi) at supersonic speeds andhigh altitude
  
                  6,000 km (3,700 mi) at low altitudes
  * Service ceiling: 19,000 m (62,000 ft) to 22,000 m (72,000 ft)
  
  Armament
  
  * Missiles: alternative loads
  * 4-6 x Kh-22
  * 2-4 x Kh-45
  * 2-4-x Ballistic missiles
  * 4-6 x Air-to-air missiles
  