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Tupolev Tu-160 Blackjack
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<blockquote data-quote="MIGUEL" data-source="post: 199130" data-attributes="member: 1054"><p><strong>HISTORY</strong>: </p><p>First Flight 19 December 1981 </p><p>Service Entry </p><p></p><p>25 April 1987 </p><p></p><p></p><p><strong>CREW</strong>: </p><p></p><p>four: pilot, co-pilot, navigator/offensive weapons operator, navigator/EW and communications operator </p><p></p><p></p><p><strong>ESTIMATED COST</strong>: </p><p></p><p>unknown </p><p></p><p></p><p><strong>AIRFOIL SECTIONS</strong>: </p><p>Wing Root unknown </p><p>Wing Tip unknown </p><p></p><p></p><p><strong>DIMENSIONS</strong>: </p><p>Length 177.50 ft (54.10 m) </p><p>Wingspan unswept: 182.75 ft (55.70 m)</p><p>swept: 116.81 ft (35.60 m) </p><p>Height 43.00 ft (13.10 m) </p><p>Wing Area 3,870 ft2 (360.0 m2) </p><p>Canard Area </p><p></p><p>not applicable </p><p></p><p></p><p><strong>WEIGHTS</strong>: </p><p>Empty 257,940 lb (117,000 kg) </p><p>Normal Takeoff 589,955 lb (267,600 kg) </p><p>Max Takeoff 606,260 lb (275,000 kg) </p><p>Fuel Capacity internal: 326,285 lb (148,000 kg)</p><p>external: none </p><p>Max Payload </p><p></p><p>36,000 lb (16,330 kg) </p><p></p><p></p><p><strong>PROPULSION</strong>: </p><p>Powerplant four Samara/ Trud NK-321 afterburning turbofans </p><p>Thrust 123, 370 lb (548.8 kN)</p><p>220,460 lb (980.6 kN) with afterburner </p><p></p><p></p><p><strong>PERFORMANCE</strong>: </p><p>Max Level Speed at altitude: 1,380 mph (2,220 km/h) at 40,000 ft (12,200 m), Mach 2.05</p><p>at sea level: 640 mph (1,030 km/k)</p><p>cruise speed: 530 mph (850 km/h) at 30,000 ft (9,145 m), Mach 0.77 </p><p>Initial Climb Rate 13,780 ft (4,200 m) / min </p><p>Service Ceiling 52,495 ft (16,000 m) </p><p>Range 6,650 nm (12,300 km) </p><p>Endurance 15 hr </p><p>g-Limits +2 </p><p></p><p></p><p><strong>ARMAMENT</strong>: </p><p>Gun none </p><p>Stations two internal bomb bays </p><p>Air-to-Surface Missile up to 12 Kh-55/AS-15 'Kent', up to 24 Kh-15P/AS-16 'Kickback' cruise missiles</p><p>reportedly to be upgraded to carry up to 12 Kh-101 or up to 12 Kh-SD cruise missiles </p><p>Bomb theoretically compatible with various free-fall nuclear or conventional bombs, but none have yet been integrated </p><p>Other unknown </p><p></p><p></p><p><strong>KNOWN VARIANTS</strong>: </p><p>Tu-160 'Blackjack-A' Production strategic bomber; approximately 30 built </p><p>Tu-160P Proposal for an interceptor armed with medium- and long-range air-to-air-missiles to escort and defend bombers; cancelled </p><p>Tu-160PP Proposal for an electronic countermeasures model to escort bombers; cancelled </p><p>Tu-160SK Proposal for a commercial variant to carry a small space vehicle named Burlak underneath the fuselage to high altitude and then launch the vehicle into low-Earth orbit </p><p></p><p></p><p><strong>KNOWN COMBAT RECORD</strong>: </p><p></p><p>none </p><p></p><p></p><p><strong>KNOWN OPERATORS</strong>: </p><p></p><p>Russia, Voyenno Vozdushniye Sili (Russian Air Force)</p><p>Ukraine, Voyenno Vozdushnyye Sily (Ukraine Military Air Forces)</p><p>Union of Soviet Socialist Republics, Voyenno Vozdushniye Sili (Soviet Air Force) </p><p></p><p></p><p><strong>3-VIEW SCHEMATIC</strong>: </p><p></p><p><img src="http://www.aerospaceweb.org/aircraft/bomber/tu160/tu160_schem_01.gif" alt="" class="fr-fic fr-dii fr-draggable " style="" /></p></blockquote><p></p>
[QUOTE="MIGUEL, post: 199130, member: 1054"] [B]HISTORY[/B]: First Flight 19 December 1981 Service Entry 25 April 1987 [B]CREW[/B]: four: pilot, co-pilot, navigator/offensive weapons operator, navigator/EW and communications operator [B]ESTIMATED COST[/B]: unknown [B]AIRFOIL SECTIONS[/B]: Wing Root unknown Wing Tip unknown [B]DIMENSIONS[/B]: Length 177.50 ft (54.10 m) Wingspan unswept: 182.75 ft (55.70 m) swept: 116.81 ft (35.60 m) Height 43.00 ft (13.10 m) Wing Area 3,870 ft2 (360.0 m2) Canard Area not applicable [B]WEIGHTS[/B]: Empty 257,940 lb (117,000 kg) Normal Takeoff 589,955 lb (267,600 kg) Max Takeoff 606,260 lb (275,000 kg) Fuel Capacity internal: 326,285 lb (148,000 kg) external: none Max Payload 36,000 lb (16,330 kg) [B]PROPULSION[/B]: Powerplant four Samara/ Trud NK-321 afterburning turbofans Thrust 123, 370 lb (548.8 kN) 220,460 lb (980.6 kN) with afterburner [B]PERFORMANCE[/B]: Max Level Speed at altitude: 1,380 mph (2,220 km/h) at 40,000 ft (12,200 m), Mach 2.05 at sea level: 640 mph (1,030 km/k) cruise speed: 530 mph (850 km/h) at 30,000 ft (9,145 m), Mach 0.77 Initial Climb Rate 13,780 ft (4,200 m) / min Service Ceiling 52,495 ft (16,000 m) Range 6,650 nm (12,300 km) Endurance 15 hr g-Limits +2 [B]ARMAMENT[/B]: Gun none Stations two internal bomb bays Air-to-Surface Missile up to 12 Kh-55/AS-15 'Kent', up to 24 Kh-15P/AS-16 'Kickback' cruise missiles reportedly to be upgraded to carry up to 12 Kh-101 or up to 12 Kh-SD cruise missiles Bomb theoretically compatible with various free-fall nuclear or conventional bombs, but none have yet been integrated Other unknown [B]KNOWN VARIANTS[/B]: Tu-160 'Blackjack-A' Production strategic bomber; approximately 30 built Tu-160P Proposal for an interceptor armed with medium- and long-range air-to-air-missiles to escort and defend bombers; cancelled Tu-160PP Proposal for an electronic countermeasures model to escort bombers; cancelled Tu-160SK Proposal for a commercial variant to carry a small space vehicle named Burlak underneath the fuselage to high altitude and then launch the vehicle into low-Earth orbit [B]KNOWN COMBAT RECORD[/B]: none [B]KNOWN OPERATORS[/B]: Russia, Voyenno Vozdushniye Sili (Russian Air Force) Ukraine, Voyenno Vozdushnyye Sily (Ukraine Military Air Forces) Union of Soviet Socialist Republics, Voyenno Vozdushniye Sili (Soviet Air Force) [B]3-VIEW SCHEMATIC[/B]: [IMG]http://www.aerospaceweb.org/aircraft/bomber/tu160/tu160_schem_01.gif[/IMG] [/QUOTE]
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