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Tu-95 (Bear) Russian Strategic Bomber Aircraft

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Basic Information
Name
Tu-95 (Bear) Russian Strategic Bomber Aircraft
Designation
Alternate Designation
Equipment Type
Manufacturer
Tupolev
Date of Introduction
1956
Description

The Tupolev Tu-95 (Russian: Туполев Ту-95; NATO reporting name: "Bear") is a large, four-engine turboprop-powered strategic bomber and missile platform. First flown in 1952, the Tu-95 entered service with the Soviet Union in 1956 and is expected to serve the Russian Aerospace Forces until at least 2040. A development of the bomber for maritime patrol is designated Tu-142, while a passenger airliner derivative was called Tu-114. The aircraft has four Kuznetsov NK-12 engines with contra-rotating propellers. It is the only propeller-powered strategic bomber still in operational use today. The Tu-95 is one of the loudest military aircraft, particularly because the tips of the propeller blades move faster than the speed of sound. Its distinctive swept-back wings are set at an angle of 35°. The Tu-95 is unique as a propeller-driven aircraft with swept wings that has been built in large numbers. The design bureau, led by Andrei Tupolev, designed the Soviet Union's first intercontinental bomber, the 1949 Tu-85, a scaled-up version of the Tu-4, a Boeing B-29 Superfortress copy. A new requirement was issued to both Tupolev and Myasishchev design bureaus in 1950: the proposed bomber had to have an un-refueled range of 8,000 km (4,970 mi)—far enough to threaten key targets in the United States. Other goals included the ability to carry an 11,000 kg (24,200 pounds) load over the target. Tupolev was faced with selecting a suitable type of powerplant: the Tu-4 showed that piston engines were not powerful enough for such a large aircraft, and the AM-3 jet engines for the proposed T-4 intercontinental jet bomber used too much fuel to give the required range. Turboprop engines were more powerful than piston engines and gave better range than the turbojets available at the time, and gave a top speed between the two. Turboprops were also initially selected for the Boeing B-52 Stratofortress to meet its long range requirement,[6] and for the British long-range transport aircraft, the Saunders-Roe Princess, the Bristol Brabazon and the Bristol Britannia. Tupolev proposed a turboprop installation and Tu-95 design with this configuration was officially approved by the government on 11 July 1951. It used four Kuznetsov coupled turboprops, each fitted with two contra-rotating propellers with four blades each, with a nominal 8,948 kW (12,000 effective shaft horse power [eshp]) power rating. The engine, advanced for its time, was designed by a German team of ex-Junkers prisoner-engineers under Ferdinand Brandner. The fuselage was conventional with a mid-mounted wing with 35 degrees of sweep, an angle which ensured that the main wing spar passed through the fuselage in front of the bomb bay. Retractable tricycle landing gear was fitted, with all three gear strut units retracting rearwards, with the main gear units retracting rearwards into extensions of the inner engine nacelles. The Tu-95/I, with 2TV-2F engines, first flew in November 1952 with test pilot Alexey Perelet at the controls.After six months of test flights this aircraft suffered a propeller gearbox failure and crashed, killing Perelet. The second aircraft, Tu-95/II used four 12,000 eshp Kuznetsov NK-12 turboprops which proved more reliable than the coupled 2TV-2F. After a successful flight testing phase, series production of the Tu-95 started in January 1956. For a long time, the Tu-95 was known to U.S./NATO intelligence as the Tu-20. While this was the original Soviet Air Force designation for the aircraft, by the time it was being supplied to operational units it was already better known under the Tu-95 designation used internally by Tupolev, and the Tu-20 designation quickly fell out of use in the USSR. Since the Tu-20 designation was used on many documents acquired by U.S. intelligence agents, the name continued to be used outside the Soviet Union. Initially the United States Department of Defense evaluated the Tu-95 as having a maximum speed of 644 km/h (400 mph) with a range of 12,500 km (7,800 mi). These numbers had to be revised upward numerous times. Like its American counterpart, the Boeing B-52 Stratofortress, the Tu-95 has continued to operate in the Russian Air Force while several subsequent iterations of bomber design have come and gone. Part of the reason for this longevity was its suitability, like the B-52, for modification to different missions. Whereas the Tu-95 was originally intended to drop free-falling nuclear weapons, it was subsequently modified to perform a wide range of roles, such as the deployment of cruise missiles, maritime patrol (Tu-142), and even civilian airliner (Tu-114). An AWACS platform (Tu-126) was developed from the Tu-114. An icon of the Cold War, the Tu-95 has served, not only as a weapons platform, but as a symbol of Soviet and later Russian national prestige. Russia's air force has received the first examples of a number of modernised strategic bombers in Tu-95MSs following upgrade work. Enhancements have been confined to the bomber's electronic weapons and targeting systems. Modernization Currently ongoing modernization of the Russia's Tu-95MS bombers is aimed primarily on the aircraft armament, namely adaptation of the new Kh-101/102 stealth cruise missile. The modernization includes installation of four underwing pylons for up to 8 Kh-101/102 cruise missiles as well as adjusting aircraft's main weapons bay for cruise missiles of size the Kh-101/102 (7.5 meters). Besides, the modernized Tu-95MS aircraft use radio-radar equipment and target-acquiring/navigation system based on GLONASS. The first Tu-95 modernized to carry the Kh-101/102 missiles was the Tu-95MS Saratov, rolled out at the Beriev aircraft plant in Taganrog in early 2015. It was transferred to the Russian Air Force in March 2015. Since 2015, the serial modernization is carried out also by the Aviakor aircraft plant in Samara at a rate of three aircraft per year. The first Tu-95 modernized by the Aviakor was the Tu-95MS Dubna, transferred to the Russian Air Force on 18 November 2015. In the future, Tu-95MSs are to be upgraded also with the new Kuznetsov NK-12MPM turboprop engines for increased flight range, combat load and reduced noise and vibrations and with the SVP-24 sighting and computing system from the Russian company Gefest & T. More complex modernization of the Tu-95MS16 bombers, known as "Tu-95MSM", is currently under development by Tupolev under a contract issued by the Russian Defence Ministry on 23 December 2009. This modernization is to include installation of the new Novella-NV1.021 radar, instead of the current Obzor-MS, installation of the SOI-021 information display system and the Meteor-NM2 airborne defense complex. In addition, the aircraft modernized to the "MSM" variant will be equipped with the upgraded Kuznetsov NK-12MPM turboprop engines. A contract for first modernized aircraft was signed in February 2018 with first flight scheduled for end of 2019.

Air & Air Defense Specifications
Crew 7
Range 11.0 km
Service Ceiling 12 m
Variants
Tu-95/1 The first prototype powered by Kuznetsov 2TV-2F coupled turboprop engines.
Tu-95/2 The second prototype powered by Kuznetsov NK-12 turboprops.
Tu-95 Basic variant of the long-range strategic bomber and the only model of the aircraft never fitted with a nose refuelling probe. Known to NATO as the Bear-A.
Tu-95K Experimental version for air-dropping a MiG-19 SM-20 jet aircraft.
Tu-95K22 Conversions of the older Bear bombers, reconfigured to carry the Raduga Kh-22 missile and incorporating modern avionics. Known to NATO as the Bear-G.
Tu-95K/Tu-95KD Designed to carry the Kh-20 air-to-surface missile. The Tu-95KD aircraft were the first to be outfitted with nose probes. Known to NATO as the Bear-B.
Tu-95KM Modified and upgraded versions of the Tu-95K, most notable for their enhanced reconnaissance systems. These were in turn converted into the Bear-G configuration. Known to NATO as the Bear-C.
Tu-95LAL Experimental nuclear-powered aircraft project.
Tu-95M Modification of the serial Tu-95 with the NK-12M engines. 19 were built.
Tu-95M-55 Missile carrier.
Tu-95MR Bear-A modified for photo-reconnaissance and produced for Naval Aviation. Known to NATO as the Bear-E.
Tu-95MS/Tu-95MS6/Tu-95MS16 Completely new cruise missile carrier platform based on the Tu-142 airframe. This variant became the launch platform of the Raduga Kh-55 cruise missile and put into serial production in 1981. Known to NATO as the Bear-H and was referred to by the U.S. military as a Tu-142 for some time in the 1980s before its true designation became known. Currently being modernized to carry the Kh-101/102 stealth cruise missiles. 21 aircraft have been modernized as of April 2019.
Tu-95MS6 Capable of carrying six Kh-55, Kh-55SM or Kh-555 cruise missiles on a rotary launcher in the aircraft's weapons bay. 32 were built.
Tu-95MS16 Fitted with four underwing pylons in addition to the rotary launcher in the fuselage, giving a maximum load of 16 Kh-55s or 14 Kh-55SMs. 56 were built.
Tu-95MSM Modernization of the "Tu-95MS16" bombers, equipped with the new Novella-NV1.021 radar, SOI-021 information display system, Meteor-NM2 airborne defense complex and upgraded Kuznetsov NK-12MPM turboprop engines. First flight scheduled for end of 2019.
Tu-95N Experimental version for air-dropping an RS ramjet powered aircraft.
Tu-95RT Variant of the basic Bear-A configuration, redesigned for maritime reconnaissance and targeting as well as electronic intelligence for service in the Soviet Naval Aviation. Known to NATO as the Bear-D.
Tu-95U Training variant, modified from surviving Bear-As but now all have been retired. Known to NATO as the Bear-T.
Tu-95V Special carrier aircraft to test-drop the largest thermonuclear weapon ever designed, the Tsar Bomba.
Tu-96 Long-range intercontinental high-altitude strategic bomber prototype, designed to climb up to 16,000–17,000 m.[51] It was a high-altitude version of the Tupolev Tu-95 aircraft with high-altitude augmented turboprop TV-16 engines and with a new, enlarged-area wing. Plant tests of the aircraft were performed with non-high altitude TV-12 engines in 1955–1956.
Tu-95 derivatives Tu-114 Airliner derivative of Tu-95. Tu-116 Tu-95 fitted with passenger cabins as a stop-gap while the Tu-114 was being developed. 2 were converted.[53] Tu-126 AEW&C derivative of Tu-114, itself derived from the Tu-95. Tu-142 Maritime reconnaissance/anti-submarine warfare derivative of Tu-95. Known to NATO as the Bear-F. Several other modifications of the basic Tu-95/Tu-142 airframe have existed, but these were largely unrecognized by Western intelligence or else never reached operational status within the Soviet military.
System
Alternate Designation(s) Tupolev Tu-95; Bear
Primary Function / Type Strategic Bomber
Manufacturer Tupolev
In Service 1956-Present
Crew 7 (pilot, copilot, navigator, navigator/weapons officer, defense systems operator, flight engineer, tail gunner) ea
Number of Engines 4
Day/Night Capable Yes
All Weather Capable Yes
Number of Pylons None (Tu-95MS Bear H) 4 (Tu-95MS16 Bear H); two inner pylons on fuselage, one outer pylon on each wing between engines)
Dimensions
Length 49.13 m
Width (Wing Span) 50.04 m
Height 13.30 m
Weight, Combat (Maximum Take Off) 185 tons
Weight, Empty 91.8 tons
Weight, In-Flight 187,000 kg, Max after refueling
Weight, Landing 135,000 kg Max
Fuselage Diameter 2.90 m
Wheel Base 14.83 m
Wheel Track 12.55 m
Wing Area 289.9 m sq
Automotive
Engine Name 4 x KKBM (Kuznetsov) NK-12MA turboprops
Number of Engines 4
Engine Power 4 x 14 795 hp
Maximum Range 11 500 km
Service Ceiling 12 km
Combat Radius 6 400 km
Propeller 8-blade AV-60 K propeller units each with 2 x 4-blade co-axial contra-rotating reversible-pitch props
Fuel, Internal 84,000 kg
Maximum Speed at Altitude 830 km/h
Maximum Speed at Sea-Level 550 km/h
Cruising Speed 735 km/h
Takeoff Speed 300 km/h at max weight
Landing Speed 275 km/h at max weight
Takeoff Roll 2,450 m
Load Limit +2 G
Range, No Refueling 5,670 nm (6,524 mi, 10,500 km) normal combat load. 3,507 nm (4,039 mi, 6,500 km) max combat load.
Range, one Refueling 7,613 nm (8,761 mi, 14,100 km)
Cannon System
System
Name Gryazev-Shipunov GSh-23
Type 23mm Autocannon
Caliber 23 mm
Basic Load INA
Location Tail Turret
Length GSh-23: 1,387 mm (4 ft 7 in) GSh-23L: 1,537 mm (5 ft 1 in)
Barrel Length 1,000 mm
Barrels 2
Weight GSh-23: 49.2 kg (108 lb) GSh-23L: 50 kg (110 lb)
Action Gast principle
Rate of Fire 3,400–3,600 rounds/min (alleged)
Muzzle Velocity 715 m/s
Effective Firing Range INA
Ammunition
Type Rifle
Caliber 23 mm
Cartridge 23x115 mm
Missile System
Missile System (Option 1)
Name Kh-101 / Kh-102
Type Air-Launched Cruise Missile
Basic Load 10
Country Russia
Proliferation Widely Proliferated
In Service 2012-Present
Basing Tu-160 Blackjack, Tu-22M3/5 Backfire C, Tu-95MS16 Bear-H, and Su-27IB
Length 7.45 m
Diameter 0.51 m
Payload 450 kg
Warhead HE, fragmentation, submunition (Kh-101), 250 kt nuclear (Kh-102)
Propulsion Turbofan
Range 2,500-2800 km
Missile System (Option 2)
Name AS-15 Kent (Also known as the Kh-55)
Type Transonic air-launched Long-Range Cruise Missile
Country Russia
Basic Load 8
Length 7.00 m
Diameter 510 mm
Span 3.25 m
Weight 1,700 kg
Configuration Similar to the U.S. Tomahawk with a torpedo- shaped body, pop-out unswept wings and tail group, probably a dorsal engine intake.
Propulsion 1 turbofan
Speed Mach 0.7
Maximum Range 1,350 nm
Warhead 200 kt nuclear (information on warhead yield varies from Russian sources, which claim a 100 kt warhead, and Western sources, which has the AS-15 Russian designated Kh-55A with a 250-kt warhead)
CEP 0.08 nm (152 m; 500 ft) est.
Flight Inertial
Launch Terrain contour matching (TERCOM) until impact
Missile System (Option 3)
Name Kh-65 missiles
Type Transonic air-launched Long-Range Cruise Missile
Basic Load 14
Note The Kh-65 missiles, which are believed to be derivatives of the AS-15 Kent.
Internal Bay
Normal Load 9,000 kg
Maximum Load 20,000 kg
Rotary Launcher MKU-6, containing 6 x AS-15 Kent missiles
Fire Control / Avionics
Fire Control System Type PRS-4 box tail gun warning and fire control radar
Fire Control Radar Clam Pipe (Obozor-MS) navigation/attack
Navigation Radar Toadstool terrain following. BAND I (8-10 GHz)
Laser Desingator INA
Radar Warning Beryoza system at nose and tail
Infrared Warning Mak system under nose
Protection
Defense System Meteor-NM system
Stealth Properties No
Heat Signature Reduction INA
Add on Armor INA
NBC Protection Yes
EW Counter Measures Jammer, Geran at nose and rear fuselage
Chaffs/Flares APP-50 50-mm dispensers in undercarriage fairings
Details
Country of Origin Russia
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
T
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
49.13 m
Width
50.04 m
Height
13.3 m
Weight
185000 kg
Operators (1)
Russia
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