Tupolev Tu-160 (러시아폭격기)

 

Tupolev Tu-160  러시아 폭격기

[진공폭탄 실험 폭격기]

 

[Russian bombers on exerciseTU-160 Blackjack]

 

Type	Strategic bomber
Manufacturer	Tupolev
Maiden flight	18 December 1981
Introduced	1987/2005 (official)
Status	In production
Primary user	Russian Air Force
Produced	Kazan Aircraft Plant
Number built	35
Developed from	Myasishchev M-18

Specifications 

General characteristics

Crew: 4 (pilot, co-pilot, bombardier, defensive systems operator)

Length: 54.1 m (177 ft 6 in)

Wingspan

Spread (20° sweep): 55.70 m (189 ft 9 in)

Swept (65° sweep): 35.60 m (116 ft 10 in)

Height: 13.10 m (43 ft 0 in)

Wing area

Spread: 400 m² (4,310 ft²)

Swept: 360 m² (3,875 ft²)

Empty weight: 110 t (242,000 lb)

Loaded weight: 267 t (590,000 lb)

Max takeoff weight: 275 t (606,000 lb)

Powerplant: 4× Kuznetsov NK-321 turbofans

Dry thrust: 137 kN (30,900 lbf) each

Thrust with afterburner: 245 kN (55,100 lbf) each

Performance

Maximum speed: Mach 2.05 (2,220 km/h, 1,380 mph) at high altitude

Combat radius: =10,500km

Maximum range: 17,400 km ()

Service ceiling: 15,000 m (49,200 ft)

Rate of climb: 70 m/s (13,780 ft/min)

Wing loading: 743 kg/m² with wings fully swept (152 lb/ft²)

Thrust/weight: 0.37

Armament

2 internal bays for 40,000 kg (88,200 lb) of ordnance, options include:

2 internal rotary launchers each holding 6× Raduga Kh-55 cruise missiles (primary armament) or 12× Raduga Kh-15 short-range nuclear missiles

 

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