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Bombers ยทTupolev

Tu-95 Bear

Soviet strategic bomber, prominent during the Cold War, extensively deployed for long-range maritime patrol and anti-submarine warfare.

Tupolev Tu-95 Bear bombers in flight
Origin country
๐Ÿ‡ท๐Ÿ‡บ Ex-USSR
First flight
1952Nov 12
Introduced
1956
Produced
500units
Avg unit price
$60 million
Active worldwide
47
Tupolev Tu-95 Bear bombers side profile drawing
Side profile ยท Tupolev Tu-95 Bear ยท length 46.2 m
Technical SpecificationsVersion: Tu-95MS Bear-H
Crew8 members
Length46.2 m (151.6 ft)
Wingspan50.1 m (164.4 ft)
Height12.1 m (39.8 ft)
Wing area310 mยฒ (3336.8 sqft)
Empty weight90,000 kg (198,416 lbs)
Max. takeoff weight188,000 kg (414,469 lbs)
Powerplant4 ร— turboprops Kuznetsov NK-12M 8,950 kW each
PerformanceVersion: Tu-95MS Bear-H
Maximum speed920 km/h (572 mph)
Operational range15,000 km (9,321 mi)
Endurance21 hours
Service ceiling13,716 m (45,000 ft)
Climb rate10.0 m/s (32.8 ft/s)
Operators โ€” 2026
ActiveOn order
Armament
Missiles payload
Live Losses TrackerUpdated daily

3 losses recorded here in the Russia-Ukraine War.

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๐Ÿ‡ฎ๐Ÿ‡ณ Indiaยท ๐Ÿ‡ท๐Ÿ‡บ Russiaยท ๐Ÿ‡บ๐Ÿ‡ฆ Ukraineยท ๐Ÿ‡ท๐Ÿ‡บ Ex-USSR

Description

The Tupolev Tu-95 (NATO reporting name "Bear") is a Soviet four-engine turboprop strategic bomber and missile launch platform designed by the Tupolev design bureau. First flown in 1952, the aircraft entered service with the Long-Range Aviation of the Soviet Air Forces in 1956. It is the only turboprop-powered strategic bomber remaining in operational service and is known for its high noise levels caused by supersonic propeller blade tips.

Development

Development began in response to a 1950 requirement for a strategic bomber with an un-refueled range of 8,000 km and an 11,000 kg payload capacity. Andrei Tupolev selected turboprop engines to balance speed and fuel consumption requirements. Government approval for the design was granted on 11 July 1951. The prototype Tu-95/I first flew in November 1952 but crashed six months later following a propeller gearbox failure. The second prototype, Tu-95/II, incorporated NK-12 turboprops, leading to series production in January 1956. The modernized Tu-95MS variant entered production in 1981.

Design

The aircraft features a mid-mounted wing with 35 degrees of sweep, positioning the main wing spar forward of the bomb bay. It is powered by four Kuznetsov NK-12 turboprop engines, each driving a set of eight-bladed contra-rotating propellers. The airframe utilizes a retractable tricycle landing gear system where all units retract rearward, with the main gear housing inside the inner engine nacelle extensions. Modernized Tu-95MSM variants incorporate Novella NV1.021 passive electronically scanned array radar, upgraded NK-12MPM engines, and new AV-60T propellers to reduce airframe vibration.

Armament

The Tu-95 carries an internal and external weapon payload of up to 15,000 kg. Defensive armament consists of two 23 mm GSh-23 autocannons mounted in a tail turret. Modernized variants utilize an internal rotary launcher carrying six Kh-55-series cruise missiles, supplemented on upgraded models by four underwing pylons capable of carrying eight external Kh-101 or Kh-102 cruise missiles.

Operational History

During the Cold War, Soviet Tu-95s conducted long-range maritime reconnaissance and Arctic strike training, and a modified airframe dropped the Tsar Bomba thermonuclear device on 30 October 1961. Strategic patrol flights were suspended in 1991 but were resumed by Russia in 2007. The bomber made its combat debut in November 2015, launching cruise missiles during the Russian intervention in Syria. Russian Aerospace Forces have since deployed Tu-95MS aircraft to launch Kh-101 missiles during the invasion of Ukraine. Ukrainian drone strikes in 2022 and 2025 damaged or destroyed several airframes at Engels-2, Belaya, and Olenya airbases.

Variants

  • Tu-95: Basic initial production variant of the strategic bomber built without a nose refueling probe.
  • Tu-95RTs: Maritime reconnaissance and targeting variant fitted with a ventral search radar radome for naval targeting.
  • Tu-95MS: Cruise missile platform based on the Tu-142 airframe, equipped with an internal rotary launcher for Kh-55 missiles.
  • Tu-95MSM: Modernized variant featuring Novella NV1.021 radar, upgraded NK-12MPM engines, and external hardpoints for Kh-101 missiles.
  • Tu-114: Commercial passenger airliner derivative developed directly from the Tu-95 design.

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Frequently Asked Questions

What type of aircraft is the Tu-95 Bear?
The Tupolev Tu-95 Bear is a bombers aircraft developed by Tupolev and entered service in 1956.
What is the maximum speed of the Tu-95 Bear?
The Tupolev Tu-95 Bear has a maximum speed of 920 km/h (571 mph).
What is the range of the Tu-95 Bear?
The Tupolev Tu-95 Bear has an operational range of 15,000 km (9,320 miles). This range can vary based on payload, altitude, and mission profile.
When did the Tu-95 Bear first fly?
The Tupolev Tu-95 Bear made its first flight on November 12, 1952. It entered operational service in 1956.
How many Tu-95 Bear have been built?
Approximately 500 units of the Tupolev Tu-95 Bear have been produced since it entered service in 1956.
Which countries operate the Tu-95 Bear?
The Tupolev Tu-95 Bear is operated by 1 countries with approximately 47 aircraft in active service. The largest operators include Russia.
How much does a Tu-95 Bear cost?
The Tupolev Tu-95 Bear has an estimated unit cost of approximately $60.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the Tu-95 Bear?
The Tupolev Tu-95 Bear has a service ceiling of 13,716 meters (45,000 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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