TU-160 it is

and what a plane! mach 2 +!
http://en.wikipedia.org/wiki/Tupolev_Tu-160http://www.airforce-technology.com/projects/tu160/
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: 110,000 kg (242,500 lb)
Loaded weight: 267,600 kg (590,000 lb)
Max takeoff weight: 275,000 kg (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
Range: 12,300 km (6,640 nm, 7,640 mi) unrefueled
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