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	<title>Sukhoi Su-47 - Revision history</title>
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	<updated>2026-08-22T02:53:19Z</updated>
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		<id>https://en.bharatpedia.org/w/index.php?title=Sukhoi_Su-47&amp;diff=428962&amp;oldid=prev</id>
		<title>Ajay Kumar: Created a new article</title>
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		<updated>2023-09-19T13:25:42Z</updated>

		<summary type="html">&lt;p&gt;Created a new article&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;{{Short description|Experimental fighter aircraft}}&lt;br /&gt;
{{About|the aircraft at one time designated S-37|the aircraft designated Su-37|Sukhoi Su-37}}&lt;br /&gt;
{{More citations needed|article|date=July 2009}}&lt;br /&gt;
&amp;lt;!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --&amp;gt;&lt;br /&gt;
{|{{Infobox aircraft begin&lt;br /&gt;
  |name = Su-47 &amp;#039;&amp;#039;Berkut&amp;#039;&amp;#039;&lt;br /&gt;
  |image = File:Sukhoi Su-47 in 2007.jpg|Sukhoi Su-47 in 2007&lt;br /&gt;
  |caption = The only Su-47 at an airshow in 2008.&lt;br /&gt;
}}{{Infobox aircraft type&lt;br /&gt;
  |type = [[Experimental aircraft]]/[[Technology demonstrator]]&lt;br /&gt;
  |manufacturer =[[Sukhoi]]&lt;br /&gt;
  |designer = [[Mikhail Pogosyan]]&lt;br /&gt;
  |first flight = 25 September 1997&lt;br /&gt;
  |introduced =&lt;br /&gt;
  |retired=&lt;br /&gt;
  |status = Cancelled&lt;br /&gt;
  |primary user = [[Russian Air Force]]&lt;br /&gt;
  |&lt;br /&gt;
  |number built = 1&lt;br /&gt;
  |unit cost = &amp;lt;!--please do not add cost numbers without providing a citation--&amp;gt;&lt;br /&gt;
  |developed from =[[Sukhoi Su-37]]&lt;br /&gt;
  |variants with their own articles =&lt;br /&gt;
}}&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
The &amp;#039;&amp;#039;&amp;#039;Sukhoi Su-47 &amp;#039;&amp;#039;Berkut&amp;#039;&amp;#039;&amp;#039;&amp;#039;&amp;#039; ({{lang-ru|Сухой Су-47 Беркут|translation=Golden Eagle}}) ([[NATO reporting name]] &amp;#039;&amp;#039;&amp;#039;Firkin&amp;#039;&amp;#039;&amp;#039;&amp;lt;ref&amp;gt;{{Cite web|title = Su-47 / S-37 Berkut|url = http://www.globalsecurity.org/military/world/russia/su-47.htm|website = www.globalsecurity.org|access-date = 2016-01-10}}&amp;lt;/ref&amp;gt;), also designated &amp;#039;&amp;#039;&amp;#039;S-32&amp;#039;&amp;#039;&amp;#039; and &amp;#039;&amp;#039;&amp;#039;S-37&amp;#039;&amp;#039;&amp;#039; (not to be confused with the twin-engined delta canard design&amp;lt;ref name=&amp;quot;SSP_fighters&amp;quot;&amp;gt;Buttler, Tony and Gordon, Yefim. &amp;quot;Soviet Secret Projects: Fighters Since 1945&amp;quot;. Midland Publishing, 2005. {{ISBN|1-85780-221-7}}.&amp;lt;/ref&amp;gt; offered by Sukhoi in the early 1990s under the designation [[Sukhoi Su-37|Su-37]]) during initial development, was a Russian experimental [[supersonic]] [[fighter aircraft|jet fighter]] developed by the [[Sukhoi|JSC Sukhoi Company]]. A distinguishing feature of the aircraft was its [[forward-swept wing]]&amp;lt;ref name=&amp;quot;airwar-ru&amp;quot;&amp;gt;[http://aeroweb.lucia.it/~agretch/RAFAQ/six5th_5.html Russian Aviation Page: Sukhoi S-37 Berkut (S-32)] {{webarchive |url=https://web.archive.org/web/20060213192427/http://aeroweb.lucia.it/~agretch/RAFAQ/six5th_5.html |date=February 13, 2006 }}&amp;lt;/ref&amp;gt; which gave the aircraft excellent agility and maneuverability. While serial production of the type never materialized and the configuration was not further pursued, the sole aircraft produced served as a technology demonstrator prototype for a number of advanced technologies later used in the 4.5 generation fighter [[Sukhoi Su-35|Su-35]] and current [[fifth-generation jet fighter]] [[Sukhoi Su-57|Su-57]].&lt;br /&gt;
&lt;br /&gt;
==Development==&lt;br /&gt;
Originally known as the S-37, Sukhoi redesignated its advanced test aircraft as the Su-47 in 2002. Officially nicknamed &amp;#039;&amp;#039;&amp;#039;&amp;#039;&amp;#039;Berkut&amp;#039;&amp;#039;&amp;#039;&amp;#039;&amp;#039; ({{lang-ru|Беркут}}) (the Russian word for the [[golden eagle]]), the Su-47 was originally built as Russia&amp;#039;s principal testbed for composite materials and sophisticated fly-by-wire control systems, as well as new airframe technologies.&lt;br /&gt;
&lt;br /&gt;
[[TsAGI]] has long been aware of the advantages of forward-swept wings, with research including the development of the [[Tsibin LL]] and study of the captured [[Junkers Ju 287]] in the 1940s. At high angles of attack, the wing tips remain retracted allowing the aircraft to retain aileron control. Conversely to more conventional rear-swept wings, forward sweep geometrically creates increased [[angle of incidence (aerodynamics)|angle of incidence]] of the outer wing sections when the wing bends under load. The wings experience higher bending moments, leading to a tendency for the wings to fail structurally at lower speeds than for a straight or aft-swept wing.&lt;br /&gt;
&lt;br /&gt;
The project was launched in 1983 on order from the Soviet Air Force. But when the USSR dissolved, funding was frozen and development continued only through funding by Sukhoi.{{cn|date=April 2022}} Like its US counterpart, the [[Grumman X-29]], the Su-47 was primarily a technology demonstrator for future Russian fighters such as the [[Sukhoi Su-57]]. The forward-swept wing configuration was ultimately not pursued because it was mainly advantageous at transonic speeds while an aft-swept wing was superior at supersonic speeds.&amp;lt;ref&amp;gt;{{Cite book |last=Butowski |first=Piotr |title=Su-57 Felon |page=13 |location=Stamford, UK |publisher=Key Books |year=2021 |isbn=978-1-913870-44-7 |url=https://shop.keypublishing.com/product/View/productCode/KB0043/Su-57%20Felon}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Design==&lt;br /&gt;
[[File:Sukhoi Su-47 outline.svg|thumb|Outline of the Sukhoi Su-47]]&lt;br /&gt;
&lt;br /&gt;
The Su-47 is of similar dimensions to previous large Sukhoi fighters, such as the [[Su-35]]. To reduce development costs, the Su-47 borrowed the forward fuselage, vertical tails, and landing gear of the [[Sukhoi Su-27|Su-27]] family. Nonetheless, the aircraft includes an internal weapons bay, and space set aside for an advanced radar.&lt;br /&gt;
&lt;br /&gt;
Like its immediate predecessor, the [[Su-37]], the Su-47 is of [[Wing configuration#Horizontal stabiliser|tandem-triple]] layout, with [[canard (aeronautics)|canards]] ahead of wings and [[tailplane]]s. The Su-47 has two tailbooms of unequal length outboard of the exhaust nozzles. And they carries rearward-facing [[radar]] and a [[Drogue parachute|breaker-chute]].&amp;lt;ref&amp;gt;{{cite web|url=https://nationalinterest.org/blog/reboot/original-russian-stealth-fighter-su-47-190729|title=The Original Russian Stealth Fighter: The Su-47|first=Sebastien|last=Roblin|access-date=2023-08-23|date=2021-07-30|publisher=[[The National Interest]]}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
===Maneuverability===&lt;br /&gt;
The Su-47 has extremely high agility at subsonic speeds, enabling the aircraft to alter its angle of attack and its flight path very quickly while retaining maneuverability in supersonic flight.{{citation needed|date=March 2023}}&lt;br /&gt;
&lt;br /&gt;
===Wings===&lt;br /&gt;
The forward-swept gives the Su-47 an unconventional appearance.  The inner portion of the wing generates a substantial part of the lift. This lift is not restricted by wingtip stall{{citation needed|date=March 2023}} and the lift-induced wingtip vortex generation is thus reduced. The [[aileron]] remain effective at the highest angles of attack, and controllability of the aircraft is retained even in the event of airflow separating from the remainder of the wings&amp;#039; surface.&lt;br /&gt;
&lt;br /&gt;
A disadvantage of such a forward-swept wing design is that it twists when  under load, resulting in greater stress on the wing than occurs with a similar straight or aft-swept wing.{{fact|date=August 2023}} This requires the wing be designed to twist as it bends—opposite to the geometric twisting.{{what|geometric twisting? who he?|date=August 2023}}  This is done by the use of composites wing skins laid-up to twist. The aircraft was initially limited to Mach 1.6. Because the forward sweep was primarily beneficial at transonic speed while losing out to aft-swept wing at supersonic speed, it was not further pursued.&lt;br /&gt;
&lt;br /&gt;
===Thrust vectoring===&lt;br /&gt;
The [[thrust vectoring]] (with PFU engine modification) of ±20° at 30°/second in pitch and yaw would have greatly supported the agility gained by other aspects of the design.&lt;br /&gt;
&lt;br /&gt;
==Specifications (Su-47)==&lt;br /&gt;
{{Aircraft specs&lt;br /&gt;
|ref=Jane&amp;#039;s All the World&amp;#039;s Aircraft 2000–01&amp;lt;ref name=JAWA00-01&amp;gt;{{cite book |title=Jane&amp;#039;s All the World&amp;#039;s Aircraft 2000–01 |editor1-last=Jackson |editor1-first=Paul|year=2000 |publisher=Jane&amp;#039;s Information Group |location=Coulsdon, Surrey, United Kingdom |isbn=978-0710620118 |edition=91st |pages=457–458}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
|prime units?=met&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
        General characteristics&lt;br /&gt;
--&amp;gt;&lt;br /&gt;
|crew=1&lt;br /&gt;
|length m=22.6&lt;br /&gt;
|length note=&lt;br /&gt;
|span m=16.7&lt;br /&gt;
|span note=&lt;br /&gt;
|height m=6.4&lt;br /&gt;
|height note=&lt;br /&gt;
|wing area sqm=56&lt;br /&gt;
|wing area note=&lt;br /&gt;
|aspect ratio=&amp;lt;!-- sailplanes --&amp;gt;&lt;br /&gt;
|airfoil=5%&lt;br /&gt;
|empty weight kg=&lt;br /&gt;
|empty weight note=&lt;br /&gt;
|gross weight kg=25670&lt;br /&gt;
|gross weight note=&lt;br /&gt;
|max takeoff weight kg=34000&lt;br /&gt;
|max takeoff weight note=&lt;br /&gt;
|fuel capacity=&lt;br /&gt;
|more general=&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
        Powerplant&lt;br /&gt;
--&amp;gt;&lt;br /&gt;
|eng1 number=2&lt;br /&gt;
|eng1 name=[[Soloviev D-30]]F6&amp;lt;ref name=Су-47&amp;gt;{{cite web|title=Су-47 (С-37) &amp;quot;Беркут&amp;quot; (Russian)|url=http://testpilot.ru/russia/sukhoi/s/37/s37.php|access-date=29 August 2020 |website=testpilot.ru}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
|eng1 type=afterburning [[turbofan]] engines&lt;br /&gt;
|eng1 kn=93.1&lt;br /&gt;
|eng1 note=engines with 2-dimensional and 3-dimensional thrust-vectoring nozzles planned for testing.&lt;br /&gt;
|eng1 kn-ab=153&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
        Performance&lt;br /&gt;
--&amp;gt;&lt;br /&gt;
|max speed kmh=2200&lt;br /&gt;
|max speed note= / M2.21 at altitude&lt;br /&gt;
::::{{cvt|1400|km/h|mph kn}} / M1.12 at sea level&lt;br /&gt;
|cruise speed kmh=&lt;br /&gt;
|cruise speed note=&lt;br /&gt;
|stall speed kmh=&lt;br /&gt;
|stall speed note=&lt;br /&gt;
|never exceed speed kmh=&lt;br /&gt;
|never exceed speed note=&lt;br /&gt;
|minimum control speed kmh=&lt;br /&gt;
|minimum control speed note=&lt;br /&gt;
|range km=3300&lt;br /&gt;
|range note=&lt;br /&gt;
|combat range km=&lt;br /&gt;
|combat range note=&lt;br /&gt;
|ferry range km=&lt;br /&gt;
|ferry range note=&lt;br /&gt;
|endurance=&amp;lt;!-- if range unknown --&amp;gt;&lt;br /&gt;
|ceiling m=18000&lt;br /&gt;
|ceiling note=&lt;br /&gt;
|g limits=&amp;lt;big&amp;gt;+&amp;lt;/big&amp;gt;9&lt;br /&gt;
|roll rate=&amp;lt;!-- aerobatic --&amp;gt;&lt;br /&gt;
|climb rate ms=233&amp;lt;ref name=&amp;quot;climb_rate&amp;quot;&amp;gt;{{cite web|title=Su-47 (S-37 Berkut) Golden Eagle Fighter |url=https://www.airforce-technology.com/projects/s37/ |access-date=25 March 2020 |website=airforce-technology.com}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
|time to altitude=&lt;br /&gt;
|wing loading kg/m2=607&lt;br /&gt;
|wing loading note=max (approx.)&lt;br /&gt;
::::{{cvt|458|kg/m2}} normal (approx.)&lt;br /&gt;
|fuel consumption kg/km=&lt;br /&gt;
|power/mass=&lt;br /&gt;
|thrust/weight=1.00 max take-off weight &amp;lt;!--see talk page--&amp;gt; &lt;br /&gt;
::::1.29 normal take-off weight &amp;lt;!--see talk page--&amp;gt; &lt;br /&gt;
|more performance=&amp;lt;!--&amp;lt;/br&amp;gt;&lt;br /&gt;
*&amp;#039;&amp;#039;&amp;#039;Take-off run:&amp;#039;&amp;#039;&amp;#039; {{cvt||m|0}}&lt;br /&gt;
*&amp;#039;&amp;#039;&amp;#039;Take-off run to {{cvt|15|m|0}}:&amp;#039;&amp;#039;&amp;#039; {{cvt||m|0}}&lt;br /&gt;
*&amp;#039;&amp;#039;&amp;#039;Landing run:&amp;#039;&amp;#039;&amp;#039; {{cvt|15|m|0}}&lt;br /&gt;
*&amp;#039;&amp;#039;&amp;#039;Landing run to {{cvt|15|m|0}}:&amp;#039;&amp;#039;&amp;#039; {{cvt||m|0}}--&amp;gt;&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
        Armament&lt;br /&gt;
--&amp;gt;&lt;br /&gt;
|armament=*provision for conformal weapon storage&lt;br /&gt;
&lt;br /&gt;
|avionics=*provision for mission radar in nose and ECM in tail radomes&lt;br /&gt;
}}&lt;br /&gt;
&lt;br /&gt;
== Gallery ==&lt;br /&gt;
&amp;lt;gallery widths=&amp;quot;215&amp;quot; heights=&amp;quot;150px&amp;quot;&amp;gt;&lt;br /&gt;
File:Sukhoi Su-47 Berkut (S-37) in 2001.jpg&lt;br /&gt;
File:Russian Air Force, 01, Sukhoi Su-47 Berkut (49581076306).jpg&lt;br /&gt;
File:Sukhoi Su-35UB and Su-47 at MAKS-2003 airshow.jpg|Su-47 next to a Sukhoi Su-35UB at the [[MAKS (air show)|MAKS-2003]] air show.&lt;br /&gt;
File:Sukhoi Su-47 in formation, 2005.jpg|Sukhoi Su-47 Berkut in the lead, followed by a Su-27SKM (top) and a Su-30MKK (bottom).&lt;br /&gt;
&amp;lt;/gallery&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
&lt;br /&gt;
{{aircontent|&lt;br /&gt;
|related=&amp;lt;!-- designs which were developed into or from this aircraft: --&amp;gt;&lt;br /&gt;
* [[Sukhoi Su-27]]&lt;br /&gt;
* [[Sukhoi Su-30]]&lt;br /&gt;
* [[Sukhoi Su-33]]&lt;br /&gt;
* [[Sukhoi Su-34]]&lt;br /&gt;
* [[Sukhoi Su-35]]&lt;br /&gt;
* [[Sukhoi Su-37]]&lt;br /&gt;
* [[Sukhoi Su-57]] / [[Sukhoi/HAL FGFA]]&lt;br /&gt;
|similar aircraft=&lt;br /&gt;
* [[KB SAT SR-10]]&lt;br /&gt;
* [[Grumman X-29]]&lt;br /&gt;
* [[Mikoyan Project 1.44]]&lt;br /&gt;
|lists=&lt;br /&gt;
|see also=&lt;br /&gt;
}}&lt;br /&gt;
&lt;br /&gt;
== References ==&lt;br /&gt;
{{Reflist}}&lt;br /&gt;
&lt;br /&gt;
== Bibliography ==&lt;br /&gt;
* {{cite book | last = Gordon| first = Yefim | title = Sukhoi S-37 and Mikoyan MFI: Russian Fifth-Generation Fighter Demonstrators – Red Star Vol. 1 | publisher = Midland Publishing| year = 2002 | isbn= 978-1-85780-120-0 }}&lt;br /&gt;
* {{cite book | last = Tayor | first = Michael J. H. | title = World Aircraft &amp;amp; Systems Directory | publisher = Brassey&amp;#039;s | year=  1999 | location = Herndon, VA | pages = 78–79 }}&lt;br /&gt;
&lt;br /&gt;
==External links==&lt;br /&gt;
&lt;br /&gt;
* [http://www.fighter-planes.com/info/s37.htm S-37 Berkut at Fighter-Planes.com]&lt;br /&gt;
&lt;br /&gt;
{{Sukhoi aircraft}}&lt;br /&gt;
{{USAF/DoD reporting names}}&lt;br /&gt;
&lt;br /&gt;
{{Authority control}}&lt;br /&gt;
&lt;br /&gt;
[[Category:1990s Soviet and Russian experimental aircraft]]&lt;br /&gt;
[[Category:1990s Soviet and Russian fighter aircraft]]&lt;br /&gt;
[[Category:Abandoned military aircraft projects of Russia]]&lt;br /&gt;
[[Category:Aircraft first flown in 1997]]&lt;br /&gt;
[[Category:Canard aircraft]]&lt;br /&gt;
[[Category:Forward-swept-wing aircraft]]&lt;br /&gt;
[[Category:Relaxed-stability aircraft]]&lt;br /&gt;
[[Category:Sukhoi aircraft|Su-47]]&lt;br /&gt;
[[Category:Twinjets]]&lt;/div&gt;</summary>
		<author><name>Ajay Kumar</name></author>
	</entry>
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