Tupolev Tu-160 Beliey Lebed atau Angsa Putih(Rusia: Туполев Ту-160, Nama NATO : Blackjack) adalah pesawat pembom supersonik sayap rendah (low wing) dengan sayap sweep variabel yang dirancang oleh Tupolev pada tahun 1980. Pesawat ini dioperasikan oleh Angkatan Udara Rusia, dengan jumlah pesawat sebanyak 16 unit.
TU-160 White Swan merupakan pesawat yang terbesar dalam sejarah penerbangan militer, untuk kategori pesawat supersonik dan pesawat dengan sayap geometri variabel. Pesawat ini juga merupakan pesawat tempur terberat di dunia yang berjenis pembom terbesar. Di antara para pilot pesawat ini dijuluki sebagai "White Swan".
Pesawat ini mulai bertugas pada tahun 1987, dan merupakan pesawat pembom strategis terakhir yang dirancang khusus untuk Uni Soviet.
Pada tanggal 17 November 2015, Rusia mulai menggunakan Tu-160, Tu-95 dan Tu-22m pembom Strategis jarak jauh terhadap sasaran di Suriah, bersama dengan rudal jelajah Kalibr ditembakkan dari Mediterania. Ini menandai debut tempur Tu-160 dan Tu-95.
Spesifikasi Tu-160 :
Crew: 4 (pilot, co-pilot, bombardier, defensive systems officer)
Length: 54.10 m (177 ft 5 in)
Wingspan:
-Spread (20° sweep): 55.70 m (182 ft 9 in)
-Swept (65° sweep): 35.60 m (116 ft 9¾ in)
-Height: 13.10 m (43 ft 0 in)
Wing area:
-Spread: 400 m² (4,306 ft²)
-Swept: 360 square metres (3,900 sq ft))
Empty weight: 110,000 kg (242,505 lb; operating empty weight)
Loaded weight: 267,600 kg (589,950 lb)
Max. takeoff weight: 275,000 kg (606,260 lb)
Powerplant: 4 × Samara NK-321 turbofans Dry thrust: 137.3 kN (30,865 lbf) each Thrust with afterburner: 245 kN (55,115 lbf) each
Performance :
-Maximum speed: Mach 2.05 (2,220 km/h, 1,200 knots, 1,380 mph) at 12,200 m (40,000 ft)
-Cruise speed: Mach 0.9 (960 km/h, 518 knots, 596 mph)
-Range: 12,300 km (7,643 mi) practical range without in-flight refuelling, Mach 0.77 and carrying 6 × -Kh-55SM dropped at mid range and 5% fuel reserves
-Combat radius: 7,300 km (3,994 nmi, 4,536 mi,) 2,000 km (1,080 nmi, 1,240 mi) at Mach 1.5 -Service ceiling: 16,000 m (51,181 ft)
-Rate of climb: 70 m/s (13,860 ft/min)
-Wing loading: 742 kg/m² with wings fully swept (152 lb/ft²)
-lift-to-drag: 18.5–19, while supersonic it is above 6 -Thrust/weight: 0.37
Persenjataan :
-Two internal bays for 40,000 kg (88,185 lb) of ordnance including
-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.
Spesifikasi Tu-160 :
Crew: 4 (pilot, co-pilot, bombardier, defensive systems officer)
Length: 54.10 m (177 ft 5 in)
Wingspan:
-Spread (20° sweep): 55.70 m (182 ft 9 in)
-Swept (65° sweep): 35.60 m (116 ft 9¾ in)
-Height: 13.10 m (43 ft 0 in)
Wing area:
-Spread: 400 m² (4,306 ft²)
-Swept: 360 square metres (3,900 sq ft))
Empty weight: 110,000 kg (242,505 lb; operating empty weight)
Loaded weight: 267,600 kg (589,950 lb)
Max. takeoff weight: 275,000 kg (606,260 lb)
Powerplant: 4 × Samara NK-321 turbofans Dry thrust: 137.3 kN (30,865 lbf) each Thrust with afterburner: 245 kN (55,115 lbf) each
Performance :
-Maximum speed: Mach 2.05 (2,220 km/h, 1,200 knots, 1,380 mph) at 12,200 m (40,000 ft)
-Cruise speed: Mach 0.9 (960 km/h, 518 knots, 596 mph)
-Range: 12,300 km (7,643 mi) practical range without in-flight refuelling, Mach 0.77 and carrying 6 × -Kh-55SM dropped at mid range and 5% fuel reserves
-Combat radius: 7,300 km (3,994 nmi, 4,536 mi,) 2,000 km (1,080 nmi, 1,240 mi) at Mach 1.5 -Service ceiling: 16,000 m (51,181 ft)
-Rate of climb: 70 m/s (13,860 ft/min)
-Wing loading: 742 kg/m² with wings fully swept (152 lb/ft²)
-lift-to-drag: 18.5–19, while supersonic it is above 6 -Thrust/weight: 0.37
Persenjataan :
-Two internal bays for 40,000 kg (88,185 lb) of ordnance including
-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.
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