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NATO reporting name: Blackjack
The Russian bomber Tu-160 Blackjack is a supersonic aircraft, variable-geometry wing heavy strategic bomber.
With the main purpose destroy target with precision nuclear and conventional weapons at the enemy at distances up to 10.000 km.
Tu-160M2 - it is a deeply modernized version of the Tu-160 (M) Blackjack. The main differences concern the cockpit, powerplant, armament warehouses of electronics board and also given great importance to the reduction of Blackjack trace.

1. It has the latest generation of electronic systems(such as: a long range navigation system and other new generation subsystems) 2. Flight refuelling probe, extended 3. consists of a four crew comprised the pilot, the co-pilot, the navigation officer and the officer weapon system 4. The structure and or wing, bring specific depths technology "Stealth" 5. The Blackjack has two weapons bay, with a total capacity of 40.000 kg 6. Power Plant NK-32 after burning turbofan engines.
The modernized version of Blackjack M2 will join service not before 2023 and will remain in service until 2063.
HIS WEAPONS:

Range: 5000-10.000 km Cruise speed: 900 km/h Service ceiling: 30-10.000 m Circle of equal probability (CEP): 5- 10 m Warhead weight (conventional head): 400 kg.

Range: 2000-5000 km Cruise speed: 900 km/h Service ceiling: 40-110 m Circle of equal probability (CEP): 5 m Warhead weight (conventional head): 410 kg.
Version:
Kh-55 («izdeliye 120» or RKB-500, AS-15)
Kh-55OK («izdeliye 124»)
Kh-55SM («izdeliye 125» or RKB-500B, AS-15b) – long range
Kh-65 – configuration of Χ-55 with conventional warhead
Kh-555 – conventionally armed version with an improved guidance system and warhead. In October 1999 he was first tested.
Three-view drawing

Technical specifications
| DESIGNER | OKB Tupolev |
| COUNTRY | Russia |
| TYPE |
Strategical bomber
|
| CREW | 4 |
| POWER-PLANT |
Four turbofan engines with afterburning Kuznetsov ΝΚ-32
|
| Thrust, kgf | |
| - with afterburning | 4x25.054 |
| - without afterburner | 4x13.990 |
|
DIMENSIONS
|
|
|
Length, m
|
55,70 |
|
Height, m
|
13,20 |
|
Wing span, m
|
|
| - with sweep 65ο | 35,65 |
| - with sweep 35ο | 50,7 |
| - with sweep 15ο | 41,7 |
| Wing area, m2 | 202,00 |
| WEIGHT | |
| Maximum take-off, kg | 275.000 |
| Normal take-off, kg | 267.600 |
| Empty aircraft, kg | 110.000 |
| Internal fuel, kg | 148.000 |
| Warload, kg | |
| - in standard configuration | 22.500 |
| - maximum | up to 40.000 |
| PERFORMANCE | |
| Maximum speed (at high altitude), km/h | 2.000 |
| Maximum speed in low height, km/h | 1.030 |
| Cruising speed, km/h | 850 |
| Range, km | |
| - with weapon load, standard configuration | 14.000 |
| - maximum weapon load | 10.500 |
| Endurance, h | +15 |
| Rate of climb, m/min | 4.200 |
| Service ceiling, m | 15.600 |
| Maximum overload, g | 2 |
| ARMAMENT | 2 drum with Cruise missiles Kh-55 and Kh-55L (Χ-55 or Χ -5M/SM (X-555 or X-101), with 12xKh-15 with nuclear and HE warhead, thermonuclear and free fall bomb, mine. |