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Tu-160 (Blackjack) Russian Strategic Bomber

Tu-160

Supersonic Strategic Bomber
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Basic Information
Name
Tu-160 (Blackjack) Russian Strategic Bomber
Designation
Tu-160
Alternate Designation
Tu-160; NATO: Blackjack (Russian designation: White Swan)
Equipment Type
Supersonic Strategic Bomber
Manufacturer
Tupolev
Date of Introduction
1987
Description

The Tupolev Tu-160 (NATO reporting name: Blackjack) is a supersonic, variable-sweep wing heavy strategic bomber designed by the Tupolev Design Bureau in the Soviet Union in the 1970s. It is the largest and heaviest Mach 2+ supersonic military aircraft ever built and next to the experimental XB-70 Valkyrie in overall length. As of 2021, it is the largest and heaviest combat aircraft, the fastest bomber in use and the largest and heaviest variable-sweep wing airplane ever flown. Entering service in 1987, the Tu-160 was the last strategic bomber designed for the Soviet Union. As of 2016, the Russian Air Force's Long Range Aviation branch has at least 16 aircraft in service. The Tu-160 active fleet has been undergoing upgrades to electronics systems since the early 2000s with the first updated aircraft delivered in December 2014.

Air & Air Defense Specifications
Crew 4
Engine Afterburning Turbofan (137 hp)
Max Speed 2.1 km/h
Service Ceiling 16000 m
Variants
Tu-160M Upgraded version that features new weaponry, improved electronics and avionics, which double its combat effectiveness.
Tu-160M2 Modernization program upgrade version featuring low observable coatings, new more powerful and efficient engines giving it greater operational range, new avionics, electronics, improved cockpit, communications and control systems, and a number of weapons, as well as improved thrust and unrefueled range. Features a new defensive system protecting it from missiles. First upgraded aircraft reportedly released in 2021.
System
Alternate Designation Tu-160; NATO: Blackjack (Russian designation: White Swan)
Type Supersonic Strategic Bomber
Manufacturer Tupolev
Crew 4 ea
Dimensions
Length 54.1 m (177 ft 6 in)
Wingspan (Wings spread) Wingspan: 55.7 m (182 ft 9 in), wings spread (20°)
Wingspan (Wings swept) 35.6 m (117 ft), wings swept (65°)
Wing Area (Wings spread) 400 m2 (4,300 sq ft) wings spread
Wing Area (Wings swept) 360 m2 (3,875 sq ft) wings swept
Height 13.1 m (43 ft 0 in)
Empty Weight 110,000 kg (242,508 lb)
Gross Weight 267,600 kg (589,957 lb)
Maximum Takeoff Weight 275,000 kg (606,271 lb)
Automotive
Engine Name 4 × Samara NK-321
Engine Type Afterburning Turbofan
Engine Power 137.3 kN (30,900 lbf) thrust each dry, 245 kN (55,000 lbf) with afterburner
Fuel Capacity INA
Maximum Speed Mach 2.05
Range 12,300 km (7,600 mi, 6,600 nmi) practical range without in-flight refueling, Mach 0.77 and carrying 6 × fuel tanks (Kh-55SM) dropped at mid range and 5% fuel reserves
Combat Range 2,000 km (1,200 mi, 1,100 nmi) at Mach 1.5; or 7,300 km (4,536 mi) at subsonic speeds
Ferry Range INA
Service Ceiling 16,000 m (52,000 ft)
Rate of Climb 70 m/s (14,000 ft/min)
Armament
Bomb Bay Two internal weapons bays for 45,000 kg (99,208 lb) of ordnance.
Missile Launchers Two internal rotary launchers each holding 6× Raduga Kh-55SM/101/102/555 cruise missiles (primary armament) or 12× AS-16 Kickback short-range nuclear missiles.
Avionics
Armament Control System Integrated aiming, navigation and flight control system
Radar Warning System Equipped
Target Navigation Radar Navigation and attack radar equipped
Protection
Stealth Properties None
Heat Signature Reduction INA
EW Countermeasures Electronic countermeasures system equipped
Chaffs/Flares INA
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
16.49 m
Width
Height
3.99 m
Weight
121381.22 kg
Operators (1)
Russia
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