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<blockquote data-quote="Hashan dis" data-source="post: 3473230" data-attributes="member: 124785"><p><strong>Su-37 Terminator, Sukhoi</strong></p><p></p><p>A derivative of the <a href="http://www.elakiri.com/forum/showthread.php?p=3473196&posted=1#post3473196" target="_blank">Su-27</a> 'Flanker', the Su-37 is a super-maneuverable thrust vectoring fighter. Designed from an <a href="http://www.fighter-planes.com/info/su35.htm" target="_blank">http://www.fighter-planes.com/info/su35.htm</a> prototype, the Su-37 test aircraft (designated T10M-11) made its maiden flight in April 1996 from the Zhukovsky flight testing center near Moscow. The Su-37 powerplant features more standard thrust than all earlier 'Flanker' variants, including the Su-35. In addition, the hydraulically actuated nozzles of its Lyulka/Saturn AL-37FU (<em><strong>F</strong>orsazh <strong>U</strong>pravlaemoye</em> meaning 'afterburning steerable') engines are steerable -15 to +15 degrees along the vertical plane. Thrust control is fully integrated into the flight control system, requiring no input from the pilot. An emergency system can automatically return the nozzles to level flight in the event of an onboard failure. The Su-37 has the newer, more powerful, NIIP NO-11M pulse-Doppler phased-array nose radar. A rearward-facing missile system and NIIP NO-12 rear-radar will give the pilot the ability to fire at enemy aircraft behind the Su-37, in addition to the front. While the Su-37 is the first Russian aircraft to feature thrust vector control comparable to that of the American <a href="http://www.fighter-planes.com/info/f22.htm" target="_blank">F-22</a>, it may not be the last. A new axisymmetrical (three-dimensional) nozzle is currently being developed by Lyulka for the future Sukhoi S-55 aircraft, a single-engined version of the Su-35. Nozzles are also being readied to make current Su-35s TVC capable. </p><p> Prime contractor: Sukhoi Design Bureau</p><p>Nation of origin: Russia</p><p> Function: Multi-role fighter</p><p>Crew: 1</p><p>Year: 1996</p><p>In-service year: ?</p><p>Engine: Two Lyulka AL-37FU vectored-thrust afterburning <a href="http://www.elakiri.com/forum/showthread.php?p=3473196&posted=1#post3473196" target="_blank">turbofans,</a> 30,855 lb thrust each</p><p>Dimensions</p><p>Wing span: 14.70 m</p><p>Length: 22.10 m </p><p>Height: 6.32 m </p><p>Weight: 40,565 lb empty / 74,956 lb max. take off</p><p>Ceiling: 59,055 ft</p><p>Speed: 2,440 km/h </p><p>Range: 3,500 km </p><p>Armament: One GSh-30-1 30mm cannon, plus up to 18,075 lb including R-73/R-77 AAMs, ASMs, bombs, rockets, drop tanks, and ECM pods carried on fourteen external points</p><p> Multi-role combat version of the Su-27, developed from the Su-35. The Su-37 uses full digital FBW controls in combination with two- dimensional thrust vectoring nozzles. Like the Su-35, it has canards. The Su-37 is not yet in production.</p><p> <strong>Type: Su-37</strong></p><p>Function: fighter</p><p>Year: 1996</p><p>Crew: 1</p><p>Engines: 2 * 137kN Saturn AL-37FU</p><p>Wing Span: 14.70 m</p><p>Length: 22.10 m</p><p>Height: 6.32 m</p><p>Wing Area: </p><p>Empty Weight: 18500 kg</p><p>Max.Weight: 34000 kg</p><p>Speed: 2400 km/h</p><p>Ceiling: 17800 m</p><p>Range: </p><p>Armament: 1*g30mm 8000 kg </p><p></p><p></p><p></p><p></p><p></p><p></p><p></p><p><img src="http://www.fighter-planes.com/5max/su37.jpg" alt="" class="fr-fic fr-dii fr-draggable " style="" /></p><p></p><p> window.google_render_ad();</p></blockquote><p></p>
[QUOTE="Hashan dis, post: 3473230, member: 124785"] [B]Su-37 Terminator, Sukhoi[/B] A derivative of the [URL="http://www.elakiri.com/forum/showthread.php?p=3473196&posted=1#post3473196"]Su-27[/URL] 'Flanker', the Su-37 is a super-maneuverable thrust vectoring fighter. Designed from an [URL="http://www.fighter-planes.com/info/su35.htm"][/URL] prototype, the Su-37 test aircraft (designated T10M-11) made its maiden flight in April 1996 from the Zhukovsky flight testing center near Moscow. The Su-37 powerplant features more standard thrust than all earlier 'Flanker' variants, including the Su-35. In addition, the hydraulically actuated nozzles of its Lyulka/Saturn AL-37FU ([I][B]F[/B]orsazh [B]U[/B]pravlaemoye[/I] meaning 'afterburning steerable') engines are steerable -15 to +15 degrees along the vertical plane. Thrust control is fully integrated into the flight control system, requiring no input from the pilot. An emergency system can automatically return the nozzles to level flight in the event of an onboard failure. The Su-37 has the newer, more powerful, NIIP NO-11M pulse-Doppler phased-array nose radar. A rearward-facing missile system and NIIP NO-12 rear-radar will give the pilot the ability to fire at enemy aircraft behind the Su-37, in addition to the front. While the Su-37 is the first Russian aircraft to feature thrust vector control comparable to that of the American [URL="http://www.fighter-planes.com/info/f22.htm"]F-22[/URL], it may not be the last. A new axisymmetrical (three-dimensional) nozzle is currently being developed by Lyulka for the future Sukhoi S-55 aircraft, a single-engined version of the Su-35. Nozzles are also being readied to make current Su-35s TVC capable. Prime contractor: Sukhoi Design Bureau Nation of origin: Russia Function: Multi-role fighter Crew: 1 Year: 1996 In-service year: ? Engine: Two Lyulka AL-37FU vectored-thrust afterburning [URL="http://www.elakiri.com/forum/showthread.php?p=3473196&posted=1#post3473196"]turbofans,[/URL] 30,855 lb thrust each Dimensions Wing span: 14.70 m Length: 22.10 m Height: 6.32 m Weight: 40,565 lb empty / 74,956 lb max. take off Ceiling: 59,055 ft Speed: 2,440 km/h Range: 3,500 km Armament: One GSh-30-1 30mm cannon, plus up to 18,075 lb including R-73/R-77 AAMs, ASMs, bombs, rockets, drop tanks, and ECM pods carried on fourteen external points Multi-role combat version of the Su-27, developed from the Su-35. The Su-37 uses full digital FBW controls in combination with two- dimensional thrust vectoring nozzles. Like the Su-35, it has canards. The Su-37 is not yet in production. [B]Type: Su-37[/B] Function: fighter Year: 1996 Crew: 1 Engines: 2 * 137kN Saturn AL-37FU Wing Span: 14.70 m Length: 22.10 m Height: 6.32 m Wing Area: Empty Weight: 18500 kg Max.Weight: 34000 kg Speed: 2400 km/h Ceiling: 17800 m Range: Armament: 1*g30mm 8000 kg [IMG]http://www.fighter-planes.com/5max/su37.jpg[/IMG] window.google_render_ad(); [/QUOTE]
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