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Sukhoi Su-37

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47: 464:, which is a two-seat fighter design that incorporated the canards, N011M radar and thrust-vectoring technology that were present and evaluated on the Su-37. In addition, through tests of the Su-27M and the Su-37, engineers had determined that thrust vectoring could compensate for the loss of manoeuvrability brought about by the removal of canards, the design of which imposed a weight penalty on the airframe. The modernized Su-35, without canards, made its first flight in February 2008. 723: 441:, Chile, as authorities sought to export the aircraft. With the expiration of the engines' service lives, the aircraft had the AL-37FUs replaced with standard production AL-31F engines which lacked movable nozzles. The loss of thrust vectoring was partially mitigated by an update to the fly-by-wire flight control system. The aircraft's foreign avionics were also replaced with indigenous designs. It resumed test flights in October 2000. 278:
the aircraft, the engine had not yet been flight-cleared. The aircraft was temporarily fitted with the less-powerful AL-31FP engine, essentially an AL-31F engine that had the AL-100 vectoring nozzles of the AL-37FU. The aircraft was rolled out in May. Two months later, the temporary engines were replaced with AL-37FUs; its nozzles could only deflect 15 degrees up or down in the
739: 230:. The aircraft crashed in December 2002 due to structural failure. The Su-37 did not enter production, despite a report in 1998 which claimed that Sukhoi had built a second Su-37 using the twelfth Su-27M airframe, T10M-11 remained the sole prototype. Sukhoi had instead applied the aircraft's systems to the design bureau's other fighter designs. 714: 386:
During the subsequent flight-test programme, the Su-37's supermaneuverability as a result of thrust-vectoring controls became apparent. According to Simonov, such a feature would allow pilots to develop new combat manoeuvres and tactics, greatly enhancing its effectiveness in dogfights. Among the new
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radar that provided the aircraft with simultaneous air-to-air and air-to-ground capability. The radar was capable of tracking twenty aerial targets and directing missiles toward eight of them simultaneously; in comparison, the Su-27M's baseline N011 could only track fifteen aerial targets and engage
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and was being used as a radar test bed. Following the airframe's completion in early 1995, the aircraft was delivered to the design bureau's experimental plant near Moscow, where engineers started installing the nozzles on the aircraft. Although Sukhoi had intended the Lyulka-Saturn AL-37FU to power
378:, Sukhoi was compelled to finance the project with its own funds; according to Simonov, the company channelled revenue from the exports of the Su-27s to China and Vietnam towards the project. The aircraft was publicly unveiled at Zhukovsky later in the year, and was redesignated Su-37. 1296:
Barrie 2003, p. 39: "While the canard layout brought advantages in terms of improved maneuverability, it also added structural weight to the airframe. A conventional airframe coupled with thrust vector control, the source said, could now provide the same
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Butowski 2004, p. 39: "The problem was solved in a similar way: removal of the canards from the airframe structure. The aircraft maneuverability will not be affected since modern control systems are much more effective than those used previously. The Su-35BM
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Apart from the addition of thrust-vectoring nozzles, the Su-37 did not outwardly differ much from the canard-equipped Su-27M. Instead, engineers had focused on the aircraft's avionics. Unlike previous Su-27Ms, the Su-37 had a digital (as opposed to analogue)
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in September 1996. Piloted by Frolov, the aircraft pitched up 180 degrees and maintained the tail-first position momentarily, which would theoretically allow the aircraft to fire a missile at a combat opponent. The Super Cobra evolved into the
1313:] will be equipped with the control system similar to the quadruple digital fly-by-wire SDU-427 system from the Su-47 Berkut experimental fighter. Additionally, the Su-35BM may also be fitted with thrust vectoring." 238:
The Sukhoi Design Bureau started research on thrust vectoring in 1983, when the Soviet government tasked the bureau with the separate development of the Su-27M. At the insistence of General Director
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in 1997. Although it was only able to perform on the last day of the show, the organisers recognised the Su-37 as the standout performer at the event. The aircraft thereafter participated in the
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Russia's Road to Corruption: How the Clinton Administration Exported Government Instead of Free Enterprise and Failed the Russian People, U. S. House of Representatives (2000), P. 204
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During test flights of the Su-27Ms, which began in 1988, engineers discovered that pilots failed to maintain active control of the aircraft at high
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at low speeds. Engineers therefore installed thrust-vectoring engines to the eleventh Su-27 (factory code T10M-11), which had been built by the
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1996, p 3: "If the pilot does not kill the opposition with his first shot, then his own aircraft's lack of energy will means [
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six of them simultaneously. The aircraft retained from the Su-27M the N012 self-defence radar located in the rearward-projecting tail boom.
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feature, the integrated propulsion and flight control systems added maneuverability at high angles of attack and low speeds. The aircraft's
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displays. The displays presented to the pilot information about navigation, systems status, and weapons selection. The pilot sat on an
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Quote: "The aircraft, Su-27 number 711, had five flights in April, apparently with the axisymmetric nozzles in a fixed configuration."
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12 hardpoints, consisting of 2 wingtip rails, and 10 wing and fuselage stations with a capacity of 8,000 kg (17,630 lb) of
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during six years of testing. The pilot Yuri Vashuk ejected safely. Despite the entry of the Su-37 into Brazilian and
410:. Nonetheless, critics have questioned the practical benefits of such manoeuvres; although they would allow an early 1701: 663: 1334: 1165: 2407: 1963: 1256: 636: 2463: 2448: 1994: 65: 46: 371: 293:, which was directly linked to the thrust-vectoring control system. Together with the aircraft's overall high 2425: 279: 266: 199: 62: 2397: 2160: 2094: 688: 332: 328: 294: 1654: 1617: 1465: 1409: 1694: 1540: 250:
vectoring nozzles. This was in contrast to the focus on two-dimensional nozzles prevailing in the West.
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Butowski, Piotr (1 November 1999). "Dominance by design: the reign of Russia's 'Flankers' – PART ONE".
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arranged in a "T" configuration; they had better backlight protection than the Su-27M's monochrome
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nozzles installed. It also had updated flight- and weapons-control systems. The aircraft made its
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afterburning turbofan engines, 83 kN (19,000 lbf) thrust each with axisymmetrical
722: 536: 374:. The nozzles were fixed during the first five flights. Due to the lack of funding from the 336: 274: 215: 2072: 2067: 2062: 2057: 1927: 1922: 1912: 1833: 1777: 1772: 1767: 744: 426: 403: 321: 262: 247: 239: 155: 150: 452:, near Moscow. The structural failure was caused by repeated exceeding of the aircraft's 532: 422: 415: 406:, thrust vectoring would have given the aircraft a considerable advantage in close-in 320:
Considerable improvement had also been made to the cockpit layout. In addition to the
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Novichkov, Nicolay (26 August 1996). "Sukhoi Set to Exploit Thrust Vector Control".
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Butowski, Piotr (10 July 1996). "Su-37 dogfights will be '10 times as effective'".
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in April 1996. Throughout the flight-test program, the Su-37 demonstrated its
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Andrews, Thomas (Spring 2003). "Su-27/30 family: 'Flanker' in the 21st Century".
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Painted in a disruptive sand and brown scheme, the aircraft was given the code
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The flight-test programme ended on 19 December 2002 when the aircraft's port
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and was demonstrated during the aircraft's international debut at the
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Experimental thrust-vectoring version of the Su-35 fighter aircraft
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2,500 km/h (1,600 mph, 1,300 kn) at high altitude
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nozzles dry, 142 kN (32,000 lbf) with afterburner
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broke off during a high-g manoeuvre, leading to it crashing at
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3,300 km (2,100 mi, 1,800 nmi) at high altitude
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manoeuvres was the Super Cobra, which was a variation of the
194:") was a single-seat twin-engine aircraft designed by the 1429:. Vol. 8. Norwalk, Connecticut: AIRtime Publishing. 817:
List of military aircraft of the Soviet Union and the CIS
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1,400 km/h (870 mph; 760 kn) at sea level
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Aircraft in fiction § Sukhoi Su-27 and derivatives
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1,390 km (860 mi; 750 nmi) at sea level
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Butowski, Piotr (Summer 2004). "Halfway to PAK FA".
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Aircraft of comparable role, configuration, and era
146: 128: 120: 115: 107: 99: 89: 79: 71: 58: 53: 39: 1645:(4541). London, UK: Reed Business Publishing: 41. 1608:(4522). London, UK: Reed Business Publishing: 16. 1506:(676). Geneva: Aerospace Media Publishing: 38–41. 1456:(4447). London, UK: Reed Business Publishing: 16. 414:, it would come at the expense of a rapid loss of 271:Komsomolsk-on-Amur Aircraft Production Association 212:Komsomolsk-on-Amur Aircraft Production Association 202:. It met the need to enhance pilot control of the 94:Komsomolsk-on-Amur Aircraft Production Association 900:This was popularly termed 'Su-37 Terminator' ... 343:that was reclined to 30 degrees to improve 1531:(4642). London: Reed Business Information: 32. 2459:1990s Soviet and Russian experimental aircraft 1633:——— (18–24 September 1996). 1376:(4). New York: McGraw-Hill: 35. 24 July 1995. 1265:(in Russian). 19 December 2002. Archived from 226:at air shows, performing manoeuvres such as a 2002: 1702: 1154:] he could present an attractive target." 1091: 1089: 8: 1225:"Sukhoi demonstrator crashes during testing" 1323:Lantratov, Constantine (20 February 2008). 34:forward-swept wing technology demonstrator. 2009: 1995: 1987: 1819: 1709: 1695: 1687: 1013: 1011: 971: 969: 305:had also been improved, as it included an 36: 2479:Three dimension thrust vectoring aircraft 886:Jane's All the World's Aircraft 2009–2010 1521:"Sukhoi flies latest Su-37 demonstrator" 1258:В Подмосковье разбился истребитель Су-35 244:Siberian Aeronautical Research Institute 103:Out of service and production, prototype 1583:(9). New York: McGraw-Hill: 50–52, 55. 1444:Barrie, Douglas (16–22 November 1994). 867: 833: 709: 1519:Gethin, Howard (9–15 September 1998). 1596:Velovich, Alexander (8–14 May 1996). 1337:from the original on 12 November 2017 421:The aircraft was demonstrated at the 299:full authority digital engine control 7: 1577:Aviation Week & Space Technology 1483:Aviation Week & Space Technology 1370:Aviation Week & Space Technology 1113:Velovich September 1996, p. 41. 994:Aviation Week & Space Technology 673:passive electronically scanned array 501:14.698 m (48 ft 3 in) 495:21.935 m (72 ft 0 in) 1504:Interavia Business & Technology 507:5.932 m (19 ft 6 in) 1682:Su-37 at Russian Military Analysis 1233:. 31 December 2002. Archived from 25: 619:230 m/s (45,000 ft/min) 358:. Following ground checks at the 1489:(9). New York: McGraw-Hill: 39. 1005:Novichkov 1996, pp. 52, 55. 737: 721: 712: 431:International Defence Exhibition 360:Gromov Flight Research Institute 45: 1196:Gordon 2007, pp. 160, 164. 1026:Gordon 2007, pp. 151, 154. 963:Gordon 2007, pp. 142, 151. 639:internal cannon with 150 rounds 525:34,000 kg (74,957 lb) 519:18,500 kg (40,786 lb) 513:62 m (670 sq ft) 2454:1990s Russian fighter aircraft 1964:2002 Sknyliv air show disaster 1635:"Slow slow, quick quick, slow" 1598:"Thrust-vectoring Su-35 flies" 1427:International Air Power Review 1095:Velovich May 1996, p. 16. 938:Gordon 2007, pp. 146–147. 604:18,800 m (61,700 ft) 282:, together or differentially. 265:due to the ineffectiveness of 1: 1164:Petrov, Ivan (25 June 1997). 805:McDonnell Douglas F/A-18 HARV 800:McDonnell Douglas F-15 ACTIVE 2489:Sukhoi Su-27 family aircraft 2474:Aircraft first flown in 1996 1174:(in Russian). Archived from 695:Notable appearances in media 458:South Korean fighter tenders 30:Not to be confused with the 1104:Novichkov 1996, p. 50. 1017:Novichkov 1996, p. 52. 954:Novichkov 1996, p. 55. 884:Jackson, Paul, ed. (2009). 795:General Dynamics F-16 VISTA 370:outside Moscow, piloted by 2505: 1446:"New Su-35 nozzles fitted" 1039:Jane's Intelligence Review 698: 664:infra-red search and track 29: 2421: 1368:"Su-35 Has New Nozzles". 1355:Gordon 2007, p. 453. 1287:Andrews 2003, p. 47. 1214:Gordon 2007, p. 172. 1205:Andrews 2003, p. 58. 1083:Gordon 2007, p. 154. 1071:Gordon 2007, p. 158. 929:Andrews 2003, p. 39. 920:Gordon 2007, p. 144. 179: 44: 1960:Accidents and incidents 1677:Su-37 at EnemyForces.com 1325: 1257: 1167:Су-37 — истребитель года 1166: 984:Barrie 1994, p. 16. 362:, the aircraft made its 2426:List of Sukhoi aircraft 2026:Fighters / interceptors 888:. Jane's. p. 515. 689:multi-function displays 678:N012 self-defence radar 480:General characteristics 333:liquid crystal displays 267:flight control surfaces 200:technology demonstrator 190:; popularly nicknamed " 66:technology demonstrator 63:Air superiority fighter 1556:Gordon, Yefim (2007). 1326:Взлетела новая "сушка" 468:Specifications (Su-37) 309:(literally "Panther") 303:weapons-control system 295:thrust-to-weight ratio 234:Design and development 134:; 28 years ago 2186:Competitive aerobatic 1125:Jane's Defence Weekly 366:on 2 April 1996 from 324:, the Su-37 had four 291:flight control system 228:360-degree somersault 1639:Flight International 1620:on 12 September 2017 1602:Flight International 1525:Flight International 1450:Flight International 1394:Flight International 1146:Flight International 1046:(11). Coulsdon, UK. 975:Gordon 2007, p. 151. 843:Flight International 224:supermaneuverability 196:Sukhoi Design Bureau 84:Sukhoi Design Bureau 911:Gethin 1998, p. 32. 752:Related development 523:Max takeoff weight: 393:Farnborough Airshow 382:Operational history 354:, later changed to 184:NATO reporting name 54:General information 32:S-37 Berkut (Su-47) 2484:Twin-tail aircraft 2408:T-12 Shturmovik-90 2381:Cancelled projects 1969:2022 Irkutsk crash 1657:on 10 October 2017 1543:on 8 November 2012 1412:on 10 October 2017 1237:on 9 November 2012 1178:on 10 October 2017 433:in Dubai, and the 368:Zhukovsky Airfield 275:country's Far East 198:which served as a 168:(Russia and China) 2434: 2433: 1984: 1983: 1872: 1871: 1567:978-1-85780-247-4 1468:on 9 October 2017 1436:978-1-880588-54-3 1390:"Deft Manoeuvres" 1269:on 5 January 2016 996:1995, p. 35. 682:Sextant Avionique 475:Gordon, Novichkov 376:Russian Air Force 326:Sextant Avionique 297:and the engine's 172: 171: 132:2 April 1996 121:Introduction date 16:(Redirected from 2496: 2104:Bombers / attack 2011: 2004: 1997: 1988: 1974:2022 Yeysk crash 1820: 1711: 1704: 1697: 1688: 1666: 1664: 1662: 1653:. 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Index

Su-37
S-37 Berkut (Su-47)

Air superiority fighter
technology demonstrator
Sukhoi Design Bureau
Komsomolsk-on-Amur Aircraft Production Association
Sukhoi Su-30MKI
Sukhoi Su-30MKM
Sukhoi Su-30SM
Sukhoi Su-35
NATO reporting name
Sukhoi Design Bureau
technology demonstrator
Su-27M
Su-27
Komsomolsk-on-Amur Aircraft Production Association
thrust-vectoring
maiden flight
supermaneuverability
360-degree somersault
Mikhail Simonov
Siberian Aeronautical Research Institute
axisymmetrical
Lyulka
Lyulka-Saturn
angles of attack
flight control surfaces
Komsomolsk-on-Amur Aircraft Production Association
country's Far East

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