Sukhoi Su-37

The Sukhoi Design Bureau started research on thrust vectoring in 1983,Gordon 2007, p. 144. when the Soviet government tasked the bureau with the separate development of the Su-27M.Andrews 2003, p. 39. At the insistence of General Director Mikhail Simonov, who had been the chief designer of the Su-27, Sukhoi and the Siberian Aeronautical Research Institute studied axisymmetrical vectoring nozzles. This was in contrast to the focus on two-dimensional nozzles prevailing in the West. Lyulka (later Lyulka-Saturn) also began studies of thrust-vectoring engines in 1985.Gordon 2007, pp. 146–147. By the late 1980s, Sukhoi were evaluating their research using its flying test beds.Novichkov 1996, p. 55.

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 angles of attack due to the ineffectiveness of flight control surfaces at low speeds. Engineers therefore installed thrust-vectoring engines to the eleventh Su-27 (factory code T10M-11), which had been built by the Komsomolsk-on-Amur Aircraft Production Association in the country's Far East and was being used as a radar test bed.Gordon 2007, pp. 142, 151. 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.{{#tag:ref|According to Flight International, engineers started installing the nozzles to the aircraft in late 1994.Barrie 1994, p. 16.|group="N"}} Although Sukhoi had intended the Lyulka-Saturn AL-37FU to power 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.Gordon 2007, p. 151. The aircraft was rolled out in May.Aviation Week & Space Technology 1995, p. 35. Two months later, the temporary engines were replaced with AL-37FUs; its nozzles could only deflect 15 degrees up or down in the pitch axis, together or differentially.Novichkov 1996, pp. 52, 55.

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) fly-by-wire flight control system, which was directly linked to the thrust-vectoring control system.Novichkov 1996, p. 52. Together with the aircraft's overall high thrust-to-weight ratio and the engine's full authority digital engine control feature, the integrated propulsion and flight control systems added maneuverability at high angles of attack and low speeds.Gordon 2007, pp. 151, 154. The aircraft's weapons-control system had also been improved, as it included an N011M Bars (literally "Panther") pulse-Doppler phased-array 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 six of them simultaneously.{{Cite journal|last=Butowski|first=Piotr|date=1 November 1999|title=Dominance by design: the reign of Russia's 'Flankers' – PART ONE|journal=Jane's Intelligence Review|location=Coulsdon, UK|volume=11|issue=11|issn=1350-6226}}Gordon 2007, p. 158. The aircraft retained from the Su-27M the N012 self-defence radar located in the rearward-projecting tail boom.

Considerable improvement had also been made to the cockpit layout. In addition to the head-up display, the Su-37 had four Sextant Avionique multi-function colour liquid crystal displays arranged in a "T" configuration; they had better backlight protection than the Su-27M's monochrome cathode-ray tube displays. The displays presented to the pilot information about navigation, systems status, and weapons selection. The pilot sat on an ejection seat that was reclined to 30 degrees to improve g-force tolerance.Gordon 2007, p. 154.

Painted in a disruptive sand and brown scheme, the aircraft was given the code 711 Blue, later changed to 711 White. Following ground checks at the Gromov Flight Research Institute, the aircraft made its maiden flight on 2 April 1996 from Zhukovsky Airfield outside Moscow, piloted by Yevgeni Frolov. The nozzles were fixed during the first five flights.{{#tag:ref|Quote: "The aircraft, Su-27 number 711, had five flights in April, apparently with the axisymmetric nozzles in a fixed configuration."|group="N"}} Due to the lack of funding from the Russian Air Force, 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.Velovich May 1996, p. 16. The aircraft was publicly unveiled at Zhukovsky later in the year, and was redesignated Su-37.

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.Novichkov 1996, p. 50. Among the new manoeuvres was the Super Cobra, which was a variation of the Pugachev's Cobra and was demonstrated during the aircraft's international debut at the Farnborough Airshow 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 kulbit (somersault), in which the Su-37 performed a 360-degree loop with an extremely tight turning radius the length of the aircraft.Velovich September 1996, p. 41. According to test pilot Anatoly Kvochur, thrust vectoring would have given the aircraft a considerable advantage in close-in dogfights.{{Cite journal|last=Butowski |first=Piotr |title=Su-37 dogfights will be '10 times as effective'|journal=Jane's Defence Weekly|location=Horley, UK|date=10 July 1996|issn=0265-3818}} Nonetheless, critics have questioned the practical benefits of such manoeuvres; although they would allow an early missile lock-on, it would come at the expense of a rapid loss of kinetic energy, which would leave the aircraft vulnerable when pilots missed their first shot.Flight International 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 {{sic}} he could present an attractive target."

The aircraft was demonstrated at the Paris Air Show 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.{{Cite news|last=Petrov|first=Ivan|script-title=ru:Су-37 — истребитель года |url=https://www.kommersant.ru/doc/179961|newspaper=Kommersant|language=ru|date=25 June 1997|access-date=10 October 2017|archive-url=https://web.archive.org/web/20171010155651/https://www.kommersant.ru/doc/179961|archive-date=10 October 2017}} The aircraft thereafter participated in the MAKS air show in Moscow, the International Defence Exhibition in Dubai, and the FIDAE air show in Santiago, Chile, as authorities sought to export the aircraft.Gordon 2007, pp. 160, 164. 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.Andrews 2003, p. 58.

The flight-test programme ended on 19 December 2002 when the aircraft's port tailplane broke off during a high-g manoeuvre, leading to it crashing at Shatura, near Moscow. The structural failure was caused by repeated exceeding of the aircraft's design load during six years of testing.Gordon 2007, p. 172. The pilot Yuri Vashuk ejected safely.{{Cite news |title=Sukhoi demonstrator crashes during testing |work=Flightglobal|date=31 December 2002 |url=http://www.flightglobal.com/news/articles/sukhoi-demonstrator-crashes-during-testing-159684/|access-date=25 August 2013 |archive-url=https://web.archive.org/web/20121109050929/http://www.flightglobal.com/news/articles/sukhoi-demonstrator-crashes-during-testing-159684/|archive-date=9 November 2012}}{{cite web|url=https://www.kommersant.ru/doc/956023|script-title=ru:В Подмосковье разбился истребитель Су-35|newspaper=Kommersant|language=ru|date=19 December 2002|access-date=16 October 2017|archive-url=https://web.archive.org/web/20160105112216/http://www.kommersant.ru/doc/956023|archive-date=5 January 2016}} Despite the entry of the Su-37 into Brazilian and South Korean fighter tenders, the aircraft failed to gain any foreign customers. India in the mid-1990s funded the development of what would result in the Su-30MKI, 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.Andrews 2003, p. 47. 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.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 capability." The modernized Su-35, without canards,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 {{sic}} 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." made its first flight in February 2008.{{Cite news|last=Lantratov|first=Constantine|script-title=ru:Взлетела новая "сушка"|url=https://www.kommersant.ru/doc/855019|newspaper=Kommersant|language=ru|date=20 February 2008|access-date=12 November 2017|archive-date=12 November 2017|archive-url=https://web.archive.org/web/20171112073904/https://www.kommersant.ru/doc/855019|url-status=live}}

{{Aircraft specs

|ref= Gordon,Gordon 2007, p. 453. Novichkov

|prime units?=met

|crew=1

|length m=21.935

|length note=

|span m=14.698

|span note=

|height m=5.932

|height note=

|wing area sqm=62

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=18500

|empty weight note=

|gross weight kg=

|gross weight note=

|max takeoff weight kg=34000

|max takeoff weight note=

|fuel capacity=

|more general=

|eng1 number=2

|eng1 name=Saturn AL-37FU

|eng1 type=afterburning turbofan engines

|eng1 kn=83

|eng1 note=with axisymmetrical thrust-vectoring nozzles

|eng1 kn-ab=142

|max speed kmh=2500

|max speed mph=1553

|max speed mach=2.35

• Mach 1.14, {{cvt|1400|km/h|mph kn}} at sea level

|max speed note=at high altitude

|cruise speed kmh=

|cruise speed note=

|stall speed kmh=

|stall speed note=

|never exceed speed kmh=

|never exceed speed note=

|minimum control speed kmh=

|minimum control speed note=

|range km=3300

|range note=at high altitude

• {{cvt|1390|km|mi nmi}} at sea level

|combat range km=

|combat range note=

|ferry range km=

|ferry range note=

|endurance=

|ceiling m=18800

|ceiling note=

|g limits=+9

|roll rate=

|climb rate ms=230

|climb rate note=

|time to altitude=

|wing loading kg/m2=

|wing loading note=

|fuel consumption kg/km=

|thrust/weight=

|more performance=

|guns=1× 30 mm GSh-30-1 internal cannon with 150 rounds

|hardpoints=12 hardpoints, consisting of 2 wingtip rails, and 10 wing and fuselage stations

|hardpoint capacity=8,000 kg (17,630 lb) of ordnance.

|hardpoint missiles=

|hardpoint bombs=

|hardpoint rockets=

|hardpoint other=

|avionics=

• OLS-35 infra-red search and track system
• N-011M Bars passive electronically scanned array radar
• N012 self-defence radar
• Sextant Avionique (Thales) LCD multi-function displays

}}

{{Main|Aircraft in fiction#Sukhoi Su-27 and derivatives}}

File:SukHoi-37.jpg|

File:Sukhoi Su-37 (14260362128).jpg

{{Portal|Aviation}}

{{aircontent

|see also=

|related=

• Sukhoi Su-27
• Sukhoi Su-30
• Sukhoi Su-33
• Sukhoi Su-34
• Sukhoi Su-35
• Sukhoi Su-47

|similar aircraft=

• General Dynamics F-16 VISTA
• McDonnell Douglas F-15 ACTIVE
• McDonnell Douglas F/A-18 HARV

|lists=

• List of military aircraft of the Soviet Union and the CIS

}}

{{reflist|group=N}}

{{Reflist|35em}}

• {{Cite journal|title=Su-35 Has New Nozzles|journal=Aviation Week & Space Technology|date=24 July 1995|page=35|volume=143|issue=4|location=New York|publisher=McGraw-Hill|issn=0005-2175}}
• {{Cite journal|title=Deft Manoeuvres|url=https://www.flightglobal.com/pdfarchive/view/1996/1996%20-%202407.html|type=commentary|journal=Flight International|date=11–17 September 1996|page=3|volume=150|issue=4540|location=London, UK|publisher=Reed Business Publishing|access-date=5 November 2017|issn=0015-3710|archive-url=https://web.archive.org/web/20171010155706/https://www.flightglobal.com/pdfarchive/view/1996/1996%20-%202407.html|archive-date=10 October 2017}}
• {{Cite book|last=Andrews|first=Thomas|date=Spring 2003|chapter=Su-27/30 family: 'Flanker' in the 21st Century|title=International Air Power Review|volume=8|location=Norwalk, Connecticut|publisher=AIRtime Publishing|isbn=978-1-880588-54-3}}
• {{Cite journal|last=Barrie|first=Douglas|title=New Su-35 nozzles fitted|url=https://www.flightglobal.com/pdfarchive/view/1994/1994%20-%202803.html|journal=Flight International|date=16–22 November 1994|page=16|volume=146|issue=4447|location=London, UK|publisher=Reed Business Publishing|access-date=5 November 2017|issn=0015-3710|archive-url=https://web.archive.org/web/20171009143850/https://www.flightglobal.com/pdfarchive/view/1994/1994%20-%202803.html|archive-date=9 October 2017}}
• {{Cite journal|last=Barrie |first=Douglas |author-mask=3|date=1 September 2003|title=Singular Demands|journal=Aviation Week & Space Technology|volume=159|issue=9|location=New York|publisher=McGraw-Hill|page=39|issn=0005-2175}}
• {{Cite journal|last=Butowski|first=Piotr|date=Summer 2004|title=Halfway to PAK FA|journal=Interavia Business & Technology|location=Geneva|publisher=Aerospace Media Publishing|issue=676|pages=38–41|issn=1423-3215}}

• {{Cite journal|first=Howard|last=Gethin|title=Sukhoi flies latest Su-37 demonstrator|journal=Flight International |location=London| publisher=Reed Business Information |date=9–15 September 1998|url=http://www.flightglobal.com/pdfarchive/view/1998/1998%20-%202468.html|access-date=26 October 2013|volume=154|issue=4642|page=32|archive-url=https://web.archive.org/web/20121108112022/http://www.flightglobal.com/pdfarchive/view/1998/1998%20-%202468.html|archive-date=8 November 2012|issn=0015-3710}}
• {{cite book|last=Gordon |first=Yefim |title=Sukhoi Su-27 |series=Famous Russian Aircraft |location= Hinckley, UK |publisher=Midlands Publishing |year= 2007 |isbn=978-1-85780-247-4}}
• {{Cite journal|last=Novichkov|first=Nicolay|title=Sukhoi Set to Exploit Thrust Vector Control|journal=Aviation Week & Space Technology|pages=50–52, 55|date=26 August 1996|volume=145|issue=9|location=New York|publisher=McGraw-Hill|issn=0005-2175}}
• {{Cite journal|last=Velovich |first=Alexander|url=https://www.flightglobal.com/pdfarchive/view/1996/1996%20-%201112.html|title=Thrust-vectoring Su-35 flies|journal=Flight International | date=8–14 May 1996 |page=16 |volume=149 |issue=4522|location=London, UK |publisher=Reed Business Publishing |access-date=5 November 2017|issn=0015-3710|archive-url=https://web.archive.org/web/20170912144618/https://www.flightglobal.com/pdfarchive/view/1996/1996%20-%201112.html|archive-date=12 September 2017}}
• {{Cite journal|last=Velovich|first=Alexander|author-mask=3|title=Slow slow, quick quick, slow|url=https://www.flightglobal.com/pdfarchive/view/1996/1996%20-%202521.html|journal=Flight International|date=18–24 September 1996|page=41|volume=150|issue=4541|location=London, UK|publisher=Reed Business Publishing|access-date=5 November 2017|issn=0015-3710|archive-url=https://web.archive.org/web/20171010155703/https://www.flightglobal.com/pdfarchive/view/1996/1996%20-%202521.html|archive-date=10 October 2017}}

{{Commons category|Sukhoi Su-37}}

• [http://www.enemyforces.com/aircraft/su37.htm Su-37 at EnemyForces.com]
• [http://www.warfare.ru/?lang=&catid=255&linkid=1607 Su-37 at Russian Military Analysis]

{{Su-27 family}}

{{Sukhoi aircraft}}

Category:1990s Russian fighter aircraft

Category:1990s Soviet and Russian experimental aircraft

Category:Aircraft first flown in 1996

Category:Aircraft with retractable tricycle landing gear

Category:Canard aircraft

Su-37

Category:Sukhoi Su-27 family aircraft

Category:Three dimension thrust vectoring aircraft

Category:Twin-tail aircraft

Category:Twinjets