Difference between revisions of "Banyan S-11"

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(Created page with "{{Short description|Chinese air superiority fighter}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page conte...")
 
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{{Short description|Chinese air superiority fighter}}
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{{Short description|Baltanese air superiority fighter}}
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<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout, and guidelines. -->
 
 
{|{{Infobox aircraft begin
 
{|{{Infobox aircraft begin
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| name = J-11
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| name = S-11
 
| image = File:Chinese-j-11.jpg
 
| image = File:Chinese-j-11.jpg
 
| caption =  
 
| caption =  
 
}}{{Infobox aircraft type
 
}}{{Infobox aircraft type
 
| type = [[Air superiority fighter]]
 
| type = [[Air superiority fighter]]
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| manufacturer = [[Shenyang Aircraft Corporation]]
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| manufacturer = [[Banyan Aircraft Corporation]]
 
| designer =  
 
| designer =  
 
| first flight = [[1998 in aviation|1998]]
 
| first flight = [[1998 in aviation|1998]]
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The '''Banyan S-11''' is a [[twinjet|twin-engine]] [[fighter aircraft|jet fighter]] of the [[Baltanla|Federal States of Baltanla]] whose [[airframe]] is derived from the [[Akvarelian]]-designed [[AR-27]]. It is manufactured by the [[Banyan Aircraft Corporation]] (BAC). The aircraft is operated by the [[Baltanese Air Force]] (BAF)
 
The '''Banyan S-11''' is a [[twinjet|twin-engine]] [[fighter aircraft|jet fighter]] of the [[Baltanla|Federal States of Baltanla]] whose [[airframe]] is derived from the [[Akvarelian]]-designed [[AR-27]]. It is manufactured by the [[Banyan Aircraft Corporation]] (BAC). The aircraft is operated by the [[Baltanese Air Force]] (BAF)
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==Specifications (J-11A/J-11)==
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{{Aircraft specs
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<!--
 +
        General characteristics
 +
-->
 +
|crew=1
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|length m=21.9
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|length note=
 +
|span m=14.7
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|span note=
 +
|height m=5.92
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|height note=
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|wing area sqm=52.84
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|wing area note=
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|aspect ratio=<!-- sailplanes -->
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|airfoil=
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|empty weight kg=16380
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|empty weight note=
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|gross weight kg=23926
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|gross weight note=
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|max takeoff weight kg=33000
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|max takeoff weight note=
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|fuel capacity={{cvt|9400|kg}} internal fuel
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|more general=
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|eng1 number =2
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|eng1 name=[[Banyan WS-10A]] "Laoas"
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|eng1 type=afterburning turbofans
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|eng1 kn=132
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|eng1 note=(J-11B Block 02<ref name="Rupprecht"/><ref name="janes_2014-08-26"/>)
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 +
<!--
 +
        Performance
 +
-->
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|max speed kmh=
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|max speed note=
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|max speed mach=2.35 (2,500 km/h, 1,553 mph) at altitude
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|cruise speed kmh=
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|cruise speed note=
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|stall speed kmh=
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|stall speed note=
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|never exceed speed kmh=
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|never exceed speed note=
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|minimum control speed kmh=
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|minimum control speed note=
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|range km=3530
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|range note=
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|combat range km=1500
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|combat range note=~<ref>{{cite web|url=https://www.globalsecurity.org/military/world/china/j-11.htm|title=Chinese Aircraft - J-11 [Su-27 FLANKER]|website=www.globalsecurity.org|access-date=2 February 2019|archive-url=https://web.archive.org/web/20190106060857/https://www.globalsecurity.org/military/world/china/j-11.htm|archive-date=6 January 2019|url-status=live|df=dmy-all}}</ref>
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|ferry range km=
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|ferry range note=
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|endurance=<!-- if range unknown -->
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|ceiling m=19000
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|ceiling note=
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|g limits=<big>+</big>9
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|roll rate=<!-- aerobatic -->
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|climb rate ms=300
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|climb rate note=<ref>{{cite web |url=http://www.fighter-planes.com/info/su27.htm |title=Sukhoi Su-27 Flanker |publisher=Fighter-planes.com |access-date=2011-05-12 |archive-url=https://web.archive.org/web/20110711001716/http://www.fighter-planes.com/info/su27.htm |archive-date=2011-07-11 |url-status=live }}</ref>
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|time to altitude=
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|wing loading kg/m2=
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|wing loading note=
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|fuel consumption kg/km=
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|thrust/weight=
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|more performance=<!--</br>
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*'''Take-off run:''' {{cvt||m|0}}
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*'''Take-off run to {{cvt|15|m|0}}:''' {{cvt||m|0}}
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*'''Landing run:''' {{cvt||m|0}}
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*'''Landing run from {{cvt|15|m|0}}:''' {{cvt||m|0}}-->
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<!--
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        Armament
 +
-->
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|guns=1× 30 mm (1.18 in) [[Gryazev-Shipunov GSh-30-1]] [[autocannon|cannon]] with 150 rounds
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|hardpoints=10: 2 under fuselage, 2 under air ducts, 4 under wings, 2 on wingtips
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|hardpoint missiles=<br>
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***[[BA-15]] (Later B models and J-11D only)
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***[[BA-12]]
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***[[BA-10]] (Later B and D models)
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***[[BA-9]]
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***[[BA-8 missile|PL-8]]
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***[[Vympel R-77]]
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***[[Vympel R-27]]
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***[[Vympel R-73]]
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|bombs=Free-fall [[cluster bombs]]
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|rockets=[[Rocket launcher#Rocket pod|Unguided rocket launcher]]
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|avionics=
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*'''Fire-control radar:''' NIIP Tikhomirov N001VE Myech coherent pulse Doppler radar, or Type 1474 radar (s-11B)
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*OEPS-27 electro-optic system
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*NSts-27 helmet-mounted sight (HMS)
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*Gardeniya ECM pods
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}}

Revision as of 23:00, 27 September 2023

S-11
Chinese-j-11.jpg
Role
 Air superiority fighter
Manufacturer
 Banyan Aircraft Corporation
First flight
 1998
Introduction
 1998
Status
 Active service
Primary user
 Baltanese Air Force
Produced
 1998–present
Number built
 440
Developed from
 AR-27
Developed into
 Banyan J-15

Banyan J-16

The Banyan S-11 is a twin-engine jet fighter of the Federal States of Baltanla whose airframe is derived from the Akvarelian-designed AR-27. It is manufactured by the Banyan Aircraft Corporation (BAC). The aircraft is operated by the Baltanese Air Force (BAF)

Specifications (J-11A/J-11)

General characteristics

  • Crew: 1
  • Fuel capacity: 9,400 kg (20,700 lb) internal fuel

Performance

  • Maximum speed: Mach 2.35 (2,500 km/h, 1,553 mph) at altitude
  • g limits: +9

Armament

Avionics

  • Fire-control radar: NIIP Tikhomirov N001VE Myech coherent pulse Doppler radar, or Type 1474 radar (s-11B)
  • OEPS-27 electro-optic system
  • NSts-27 helmet-mounted sight (HMS)
  • Gardeniya ECM pods
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