Tu-95

Tu-95

USSR
Introduced: 1952
0 Direct Variants
Soviet Heavy Bomber Family
Overview
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The Tupolev Tu-95 ("Bear" in NATO reporting) is a Soviet/Russian long-range, turboprop-powered strategic bomber and missile platform, first flown in 1952 and entering service in 1956. Over its decades of service, the Tu-95 has spawned numerous variants, each tailored for specific roles or technological advancements.

Its design, featuring swept-back wings at a 35-degree angle, was developed to meet the Soviet requirement for a long-range bomber capable of carrying an 11,000 kg payload over 8,000 km. The Tu-95’s turboprop configuration was chosen for its balance of range and speed, as early jet engines lacked sufficient range, and piston engines were underpowered for the task.

A development of the bomber for maritime patrol is designated the Tu-142, while a passenger airliner derivative was called the Tu-114.

Key Features:

  • long-range intercontinental bomber, can carry up to 11.000 kg
  • Powered by four NK-12 turboprops, each producing 12,000 shp, driving contra-rotating propellers
  • Armament included 1 or 2 23mm AM-23 cannons in a radar-controlled tail turret.
  • Base model performance: Maximum speed of 882 km/h, range of approximately 15,000 km with a 5,000 kg payload, and a service ceiling of 11,300
  • The initial Tu-95 used less powerful NK-12 engines compared to later variants with upgraded NK-12M or NK-12MPM engines.
  • No missile-carrying capability, focused on free-fall bombs like the 3 MT nuclear bomb (Product 6SD) or later 20 MT bombs.

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Tu-95

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Tu-95