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
316:
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
277:
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
1306:
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
285:
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)
395:
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
425:
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
243:
816:
2458:
874:
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
2478:
270:
211:
93:
1224:
402:(somersault), in which the Su-37 performed a 360-degree loop with an extremely tight turning radius the length of the aircraft. According to test pilot
2008:
1634:
1597:
1445:
1389:
261:
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
1520:
2453:
269:
at low speeds. Engineers therefore installed thrust-vectoring engines to the eleventh Su-27 (factory code T10M-11), which had been built by the
1708:
258:) also began studies of thrust-vectoring engines in 1985. By the late 1980s, Sukhoi were evaluating their research using its flying test beds.
2488:
2473:
1565:
1434:
298:
1148:
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 [
317:
six of them simultaneously. The aircraft retained from the Su-27M the N012 self-defence radar located in the rearward-projecting tail boom.
301:
feature, the integrated propulsion and flight control systems added maneuverability at high angles of attack and low speeds. The aircraft's
1968:
672:
339:
displays. The displays presented to the pilot information about navigation, systems status, and weapons selection. The pilot sat on an
1973:
893:
855:
Quote: "The aircraft, Su-27 number 711, had five flights in April, apparently with the axisymmetric nozzles in a fixed configuration."
430:
359:
1234:
799:
460:, the aircraft failed to gain any foreign customers. India in the mid-1990s funded the development of what would result in the
290:
645:
12 hardpoints, consisting of 2 wingtip rails, and 10 wing and fuselage stations with a capacity of 8,000 kg (17,630 lb) of
2001:
1843:
1823:
1038:
2483:
804:
794:
456:
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:
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1540:
250:
vectoring nozzles. This was in contrast to the focus on two-dimensional nozzles prevailing in the West.
1036:
Butowski, Piotr (1 November 1999). "Dominance by design: the reign of Russia's 'Flankers' – PART ONE".
842:
223:
195:
83:
2315:
2310:
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457:
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arranged in a "T" configuration; they had better backlight protection than the Su-27M's monochrome
310:
302:
183:
218:
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
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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
2442:
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1937:
1932:
1863:
1858:
1853:
411:
363:
340:
219:
1575:
Novichkov, Nicolay (26 August 1996). "Sukhoi Set to
Exploit Thrust Vector Control".
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1229:
1123:
Butowski, Piotr (10 July 1996). "Su-37 dogfights will be '10 times as effective'".
782:
777:
772:
767:
762:
757:
681:
325:
313:
222:
in April 1996. Throughout the flight-test program, the Su-37 demonstrated its
210:. The sole example built was originally the eleventh Su-27M (T10M-11) built by the
203:
165:
160:
31:
1425:
Andrews, Thomas (Spring 2003). "Su-27/30 family: 'Flanker' in the 21st
Century".
418:, which would leave the aircraft vulnerable when pilots missed their first shot.
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2280:
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2270:
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Painted in a disruptive sand and brown scheme, the aircraft was given the code
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1613:
1588:
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1511:
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1381:
1132:
1051:
444:
The flight-test programme ended on 19 December 2002 when the aircraft's port
445:
461:
438:
407:
846:, engineers started installing the nozzles to the aircraft in late 1994.
1400:(4540). London, UK: Reed Business Publishing: 3. 11–17 September 1996.
1324:
1266:
1175:
449:
344:
1686:
713:
391:
and was demonstrated during the aircraft's international debut at the
2017:
1717:
398:
251:
227:
17:
27:
Experimental thrust-vectoring version of the Su-35 fighter aircraft
1986:
434:
207:
554:
2,500 km/h (1,600 mph, 1,300 kn) at high altitude
539:
nozzles dry, 142 kN (32,000 lbf) with afterburner
1990:
1690:
448:
broke off during a high-g manoeuvre, leading to it crashing at
242:, who had been the chief designer of the Su-27, Sukhoi and the
1560:. Famous Russian Aircraft. Hinckley, UK: Midlands Publishing.
1481:——— (1 September 2003). "Singular Demands".
1309:
1150:
685:
579:
3,300 km (2,100 mi, 1,800 nmi) at high altitude
387:
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
565:
1,400 km/h (870 mph; 760 kn) at sea level
701:
Aircraft in fiction § Sukhoi Su-27 and derivatives
590:
1,390 km (860 mi; 750 nmi) at sea level
1502:
Butowski, Piotr (Summer 2004). "Halfway to PAK FA".
950:
948:
946:
944:
206:(later renamed Su-35), a further development of the
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2364:
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2232:
2211:
2185:
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2103:
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1953:
1876:
1842:
1822:
1813:
1728:
1079:
1077:
1067:
1065:
1063:
1061:
789:
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:. Archived from
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1616:. Archived from
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1550:
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1539:. Archived from
1515:
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1464:. Archived from
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1408:. Archived from
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602:Service ceiling:
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537:thrust-vectoring
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389:Pugachev's Cobra
337:cathode ray tube
263:angles of attack
216:thrust-vectoring
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49:
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21:
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429:in Moscow, the
412:missile lock-on
404:Anatoly Kvochur
384:
322:head-up display
240:Mikhail Simonov
236:
164:
159:
156:Sukhoi Su-30MKM
154:
151:Sukhoi Su-30MKI
138:
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124:25 October 1997
72:National origin
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435:FIDAE air show
423:Paris Air Show
416:kinetic energy
383:
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372:Yevgeni Frolov
329:multi-function
248:axisymmetrical
235:
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214:before having
170:
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161:Sukhoi Su-30SM
148:
147:Developed into
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811:Related lists
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341:ejection seat
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311:pulse-Doppler
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256:Lyulka-Saturn
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220:maiden flight
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2436:
2365:Agricultural
2320:
2316:Su-17 (1949)
2311:Su-15 (1949)
2301:Su-11 (1946)
2254:Experimental
2245:Superjet 100
1907:
1804:
1659:. Retrieved
1655:the original
1642:
1638:
1622:. Retrieved
1618:the original
1605:
1601:
1580:
1576:
1558:Sukhoi Su-27
1557:
1545:. Retrieved
1541:the original
1528:
1524:
1503:
1486:
1482:
1470:. Retrieved
1466:the original
1453:
1449:
1426:
1414:. Retrieved
1410:the original
1397:
1393:
1373:
1369:
1362:Bibliography
1351:
1339:. Retrieved
1330:
1318:
1308:
1302:
1297:capability."
1292:
1283:
1271:. Retrieved
1267:the original
1262:
1251:
1239:. Retrieved
1235:the original
1230:Flightglobal
1228:
1219:
1210:
1201:
1192:
1180:. Retrieved
1176:the original
1171:
1159:
1149:
1145:
1141:
1124:
1118:
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1100:
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916:
907:
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885:
879:
870:
851:
841:
836:
810:
809:
788:
787:
783:Sukhoi Su-47
778:Sukhoi Su-35
773:Sukhoi Su-34
768:Sukhoi Su-33
763:Sukhoi Su-30
758:Sukhoi Su-27
751:
750:
654:
652:
642:
632:
624:
622:
616:
607:
601:
576:
551:
544:
542:
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479:
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471:
443:
420:
397:
385:
355:
351:
349:
347:tolerance.
319:
314:phased-array
284:
260:
237:
191:
187:
176:Sukhoi Su-37
175:
173:
166:Sukhoi Su-35
129:First flight
108:Number built
2291:Su-9 (1946)
2281:Su-7 (1944)
1341:12 November
670:N-011M Bars
643:Hardpoints:
545:Performance
529:Powerplant:
454:design load
288:fly-by-wire
2443:Categories
2233:Transports
1816:production
1661:5 November
1624:5 November
1547:26 October
1472:5 November
1416:5 November
1331:Kommersant
1307: [
1273:16 October
1263:Kommersant
1182:10 October
1172:Kommersant
823:References
511:Wing area:
307:N011M Bars
280:pitch axis
192:Terminator
178:(Russian:
158:(Malaysia)
139:1996-04-02
1651:0015-3710
1614:0015-3710
1589:0005-2175
1537:0015-3710
1512:1423-3215
1495:0005-2175
1462:0015-3710
1406:0015-3710
1382:0005-2175
1241:25 August
1133:0265-3818
1052:1350-6226
863:Citations
828:Footnotes
684:(Thales)
635:1× 30 mm
608:g limits:
499:Wingspan:
473:Data from
446:Tailplane
408:dogfights
356:711 White
188:Flanker-F
2469:Twinjets
2212:Trainers
2020:aircraft
1945:Fullback
1844:Shenyang
1834:Su-30MKI
1729:Aircraft
1335:Archived
731:See also
655:Avionics
647:ordnance
637:GSh-30-1
625:Armament
462:Su-30MKI
439:Santiago
352:711 Blue
246:studied
180:Сухой Су
163:(Russia)
90:Built by
80:Designer
1928:H (III)
1888:Flanker
1847:(China)
1827:(India)
1814:Foreign
706:Gallery
662:OLS-35
505:Height:
493:Length:
450:Shatura
345:g-force
331:colour
273:in the
254:(later
153:(India)
137: (
116:History
2388:KR-860
2018:Sukhoi
1954:Topics
1923:H (II)
1723:family
1718:Sukhoi
1649:
1612:
1587:
1564:
1535:
1510:
1493:
1460:
1433:
1404:
1380:
1131:
1050:
892:
666:system
577:Range:
399:kulbit
252:Lyulka
204:Su-27M
100:Status
75:Russia
2403:T-60S
2372:Su-38
2356:T-431
2351:T-405
2326:Su-47
2321:Su-37
2306:Su-13
2296:Su-10
2240:Su-80
2224:Su-29
2219:Su-28
2203:Su-31
2198:Su-29
2193:Su-26
2177:Su-12
2156:Su-39
2151:Su-34
2146:Su-25
2141:Su-24
2136:Su-22
2131:Su-20
2126:Su-17
2095:Su-75
2090:Su-57
2085:Su-35
2080:Su-33
2053:Su-30
2048:Su-27
2043:Su-15
2038:Su-11
1918:H (I)
1805:Su-37
1800:Su-35
1795:Su-34
1790:Su-33
1785:Su-32
1763:Su-30
1758:Su-29
1753:Su-28
1736:Su-27
1721:Su-27
675:radar
633:Guns:
487:Crew:
208:Su-27
182:-37;
40:Su-37
18:Su-37
2398:S-21
2346:T-49
2286:Su-8
2276:Su-6
2271:Su-5
2266:Su-3
2261:Su-1
2121:Su-7
2116:Su-4
2111:Su-2
2033:Su-9
1878:NATO
1864:J-16
1859:J-15
1854:J-11
1663:2017
1647:ISSN
1626:2017
1610:ISSN
1585:ISSN
1562:ISBN
1549:2013
1533:ISSN
1508:ISSN
1491:ISSN
1474:2017
1458:ISSN
1431:ISBN
1418:2017
1402:ISSN
1378:ISSN
1343:2017
1275:2017
1243:2013
1184:2017
1129:ISSN
1048:ISSN
890:ISBN
531:2 ×
174:The
59:Type
2393:S-6
2341:T-4
2336:T-3
2331:P-1
2073:MKM
2068:MKK
2063:MKI
2058:MKA
1824:HAL
1778:MKM
1773:MKK
1768:MKA
1643:150
1606:149
1581:145
1529:154
1487:159
1454:146
1398:150
1374:143
1310:sic
1151:sic
686:LCD
437:in
2445::
1938:X2
1641:.
1637:.
1604:.
1600:.
1579:.
1527:.
1523:.
1485:.
1452:.
1448:.
1392:.
1372:.
1329:.
1261:.
1227:.
1170:.
1088:^
1076:^
1060:^
1044:11
1042:.
1010:^
968:^
943:^
898:.
186::
2010:e
2003:t
1996:v
1933:L
1913:G
1908:F
1903:E
1898:D
1893:C
1746:M
1741:K
1710:e
1703:t
1696:v
1665:.
1628:.
1591:.
1570:.
1551:.
1514:.
1497:.
1476:.
1439:.
1420:.
1384:.
1345:.
1277:.
1245:.
1186:.
1135:.
1054:.
649:.
613:9
611:+
489:1
141:)
111:1
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.