moji5
10th August 2010, 12:18 PM
Tupolev Tu-160 Blackjack
Long-range strategic bomber
http://www.military-today.com/aircraft/tupolev_tu160_blackjack.jpg
http://uc-njavan.ir/images/781s3w3za4vztcrt6oct.jpg
سایر تصاویر
http://www.aerospaceweb.org/aircraft/bomber/tu160/tu160_schem_01.gif
Tu-160 panelhttp://www.aerospaceweb.org/aircraft/cockpits/tu160/tu160_panel_01.jpg
Tupolev Tu-22M3
http://aces.safarikovi.org/victories/obr1/aircraft_tu-22m3_russia.jpg
http://aces.safarikovi.org/victories/obr1/russia_tu-22.jpg
Tupolev Tu-22M3
The Tupolev Tu-22 (http://en.wikipedia.org/wiki/Tupolev_Tu-22) had not proved particularly successful, in some respects being inferior to the earlier Tu-16 (http://en.wikipedia.org/wiki/Tupolev_Tu-16). Its range and take-off performance, in particular, were definite weak points. Even as the Tu-22 was entering service, OKB Tupolev began work on an improved successor.
As with the contemporary MiG-23 (http://en.wikipedia.org/wiki/Mikoyan-Gurevich_MiG-23) and Su-17 (http://en.wikipedia.org/wiki/Sukhoi_Su-17) projects, the advantages of variable-geometry (http://en.wikipedia.org/wiki/Swing-wing) wings seemed attractive, allowing a combination of short take-off performance, efficient cruising, and good high-speed, low-level ride. The result was a new swing-wing aircraft called Samolyot 145, derived from the Tu-22, with some features borrowed from the abortive Tu-98 (http://en.wikipedia.org/wiki/Tupolev_Tu-98). The Tu-22M was based on the Tu-22's weapon system and used its Kh-22 (http://en.wikipedia.org/wiki/Raduga_Kh-22) missile. The Tu-22M designation was used to help get approval for the bomber within the Soviet system.[1] (http://en.wikipedia.org/wiki/Tupolev_Tu-22M#cite_note-Eden-0)
The first prototype, Tu-22M0, first flew on 30 August 1969. The resultant aircraft was first seen by NATO (http://en.wikipedia.org/wiki/NATO) around that time. For several years it was believed in the West that its service designation was Tu-26. During the SALT (http://en.wikipedia.org/wiki/SALT) negotiations of the 1980s the Soviets insisted it was the Tu-22M. At the time, Western authorities suspected that the misleading designation was intended to suggest that it was simply a derivative of the Tu-22 rather than the more advanced and capable weapon it actually was.
http://upload.wikimedia.org/wikipedia/commons/thumb/d/d1/Tupolev_Tu-22M1_refuelling_probe.jpg/800px-Tupolev_Tu-22M1_refuelling_probe.jpg (http://upload.wikimedia.org/wikipedia/commons/d/d1/Tupolev_Tu-22M1_refuelling_probe.jpg)
General characteristics
Crew: 4 (pilot, co-pilot, bombardier, defensive systems operator)
Length: 42.4 m (139 ft)
Wingspan (http://en.wikipedia.org/wiki/Wingspan):
Spread (20° sweep): 34.28 m (112 ft 6 in)
Swept (65° sweep): 23.30 m (76 ft 5 in))
Height: 11.05 m (36 ft 3 in)
Wing area:
Spread: 183.6 m² (1,976 ft²)
Swept: 175.8 m² (1,892 ft²)
Empty weight: 58,000 kg (172,000 lb)
Loaded weight: 112,000 kg (247,000 lb)
Max takeoff weight (http://en.wikipedia.org/wiki/Maximum_Takeoff_Weight): 126,000 kg (277,800 lb)
Powerplant: 2× Kuznetsov NK-25 (http://en.wikipedia.org/wiki/Kuznetsov_NK-25) turbofans (http://en.wikipedia.org/wiki/Turbofan), 245 kN (50,000 lbf) each
Performance
Maximum speed (http://en.wikipedia.org/wiki/V_speeds#Vno): Mach 2.05 (2,327 km/h,)
Range (http://en.wikipedia.org/wiki/Range_%28aircraft%29): 7,000 km (4,971 mi)
Combat radius (http://en.wikipedia.org/wiki/Combat_radius): 2,410 km (1,500 mi)
Service ceiling (http://en.wikipedia.org/wiki/Ceiling_%28aeronautics%29): 13,300 m (40,635 ft)
Rate of climb (http://en.wikipedia.org/wiki/Rate_of_climb): 15m/s (91ft/s)
Wing loading (http://en.wikipedia.org/wiki/Wing_loading): 688 kg/m² (147 lb/ft²)
Thrust/weight (http://en.wikipedia.org/wiki/Thrust-to-weight_ratio): 0.40
Armament
Guns: 1 × 23 mm GSh-23 (http://en.wikipedia.org/wiki/Gryazev-Shipunov_GSh-23L) cannon (http://en.wikipedia.org/wiki/Autocannon) in remotely controlled tail turret
Hardpoints (http://en.wikipedia.org/wiki/Hardpoint): wing and fuselage pylons and internal weapons bay with a capacity of 21,000 kg (46,300 lb) of
From up to 3 × Raduga Kh-22 (http://en.wikipedia.org/wiki/Raduga_Kh-22) missiles in weapons bay and on wing pylons or
The Tu-22M3 can carry six missiles on a MKU-6-1 rotary launcher in its bomb bay, plus four missiles on two underwing pylons for a total of ten missiles per aircraft.or
Various freefall bombs - 69 × FAB-250 (http://en.wikipedia.org/w/index.php?title=FAB-250&action=edit&redlink=1) or 8 × FAB-1500 (http://en.wikipedia.org/w/index.php?title=FAB-1500&action=edit&redlink=1) might be typical.
The Kh-55 (http://en.wikipedia.org/wiki/Kh-55) (AS-16 'Kent') long-range cruise missile was tested on the Tu-22M[9] (http://en.wikipedia.org/wiki/Tupolev_Tu-22M#cite_note-8) but apparently not used in service.
گرداورنده انجمن نخبگان جوان
Long-range strategic bomber
http://www.military-today.com/aircraft/tupolev_tu160_blackjack.jpg
http://uc-njavan.ir/images/781s3w3za4vztcrt6oct.jpg
سایر تصاویر
http://www.aerospaceweb.org/aircraft/bomber/tu160/tu160_schem_01.gif
Tu-160 panelhttp://www.aerospaceweb.org/aircraft/cockpits/tu160/tu160_panel_01.jpg
Tupolev Tu-22M3
http://aces.safarikovi.org/victories/obr1/aircraft_tu-22m3_russia.jpg
http://aces.safarikovi.org/victories/obr1/russia_tu-22.jpg
Tupolev Tu-22M3
The Tupolev Tu-22 (http://en.wikipedia.org/wiki/Tupolev_Tu-22) had not proved particularly successful, in some respects being inferior to the earlier Tu-16 (http://en.wikipedia.org/wiki/Tupolev_Tu-16). Its range and take-off performance, in particular, were definite weak points. Even as the Tu-22 was entering service, OKB Tupolev began work on an improved successor.
As with the contemporary MiG-23 (http://en.wikipedia.org/wiki/Mikoyan-Gurevich_MiG-23) and Su-17 (http://en.wikipedia.org/wiki/Sukhoi_Su-17) projects, the advantages of variable-geometry (http://en.wikipedia.org/wiki/Swing-wing) wings seemed attractive, allowing a combination of short take-off performance, efficient cruising, and good high-speed, low-level ride. The result was a new swing-wing aircraft called Samolyot 145, derived from the Tu-22, with some features borrowed from the abortive Tu-98 (http://en.wikipedia.org/wiki/Tupolev_Tu-98). The Tu-22M was based on the Tu-22's weapon system and used its Kh-22 (http://en.wikipedia.org/wiki/Raduga_Kh-22) missile. The Tu-22M designation was used to help get approval for the bomber within the Soviet system.[1] (http://en.wikipedia.org/wiki/Tupolev_Tu-22M#cite_note-Eden-0)
The first prototype, Tu-22M0, first flew on 30 August 1969. The resultant aircraft was first seen by NATO (http://en.wikipedia.org/wiki/NATO) around that time. For several years it was believed in the West that its service designation was Tu-26. During the SALT (http://en.wikipedia.org/wiki/SALT) negotiations of the 1980s the Soviets insisted it was the Tu-22M. At the time, Western authorities suspected that the misleading designation was intended to suggest that it was simply a derivative of the Tu-22 rather than the more advanced and capable weapon it actually was.
http://upload.wikimedia.org/wikipedia/commons/thumb/d/d1/Tupolev_Tu-22M1_refuelling_probe.jpg/800px-Tupolev_Tu-22M1_refuelling_probe.jpg (http://upload.wikimedia.org/wikipedia/commons/d/d1/Tupolev_Tu-22M1_refuelling_probe.jpg)
General characteristics
Crew: 4 (pilot, co-pilot, bombardier, defensive systems operator)
Length: 42.4 m (139 ft)
Wingspan (http://en.wikipedia.org/wiki/Wingspan):
Spread (20° sweep): 34.28 m (112 ft 6 in)
Swept (65° sweep): 23.30 m (76 ft 5 in))
Height: 11.05 m (36 ft 3 in)
Wing area:
Spread: 183.6 m² (1,976 ft²)
Swept: 175.8 m² (1,892 ft²)
Empty weight: 58,000 kg (172,000 lb)
Loaded weight: 112,000 kg (247,000 lb)
Max takeoff weight (http://en.wikipedia.org/wiki/Maximum_Takeoff_Weight): 126,000 kg (277,800 lb)
Powerplant: 2× Kuznetsov NK-25 (http://en.wikipedia.org/wiki/Kuznetsov_NK-25) turbofans (http://en.wikipedia.org/wiki/Turbofan), 245 kN (50,000 lbf) each
Performance
Maximum speed (http://en.wikipedia.org/wiki/V_speeds#Vno): Mach 2.05 (2,327 km/h,)
Range (http://en.wikipedia.org/wiki/Range_%28aircraft%29): 7,000 km (4,971 mi)
Combat radius (http://en.wikipedia.org/wiki/Combat_radius): 2,410 km (1,500 mi)
Service ceiling (http://en.wikipedia.org/wiki/Ceiling_%28aeronautics%29): 13,300 m (40,635 ft)
Rate of climb (http://en.wikipedia.org/wiki/Rate_of_climb): 15m/s (91ft/s)
Wing loading (http://en.wikipedia.org/wiki/Wing_loading): 688 kg/m² (147 lb/ft²)
Thrust/weight (http://en.wikipedia.org/wiki/Thrust-to-weight_ratio): 0.40
Armament
Guns: 1 × 23 mm GSh-23 (http://en.wikipedia.org/wiki/Gryazev-Shipunov_GSh-23L) cannon (http://en.wikipedia.org/wiki/Autocannon) in remotely controlled tail turret
Hardpoints (http://en.wikipedia.org/wiki/Hardpoint): wing and fuselage pylons and internal weapons bay with a capacity of 21,000 kg (46,300 lb) of
From up to 3 × Raduga Kh-22 (http://en.wikipedia.org/wiki/Raduga_Kh-22) missiles in weapons bay and on wing pylons or
The Tu-22M3 can carry six missiles on a MKU-6-1 rotary launcher in its bomb bay, plus four missiles on two underwing pylons for a total of ten missiles per aircraft.or
Various freefall bombs - 69 × FAB-250 (http://en.wikipedia.org/w/index.php?title=FAB-250&action=edit&redlink=1) or 8 × FAB-1500 (http://en.wikipedia.org/w/index.php?title=FAB-1500&action=edit&redlink=1) might be typical.
The Kh-55 (http://en.wikipedia.org/wiki/Kh-55) (AS-16 'Kent') long-range cruise missile was tested on the Tu-22M[9] (http://en.wikipedia.org/wiki/Tupolev_Tu-22M#cite_note-8) but apparently not used in service.
گرداورنده انجمن نخبگان جوان