چنگدو جی-۱۰: تفاوت میان نسخهها
محتوای حذفشده محتوای افزودهشده
ابرابزار |
ابرابزار، اصلاح ارقام |
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خط ۳۸:
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{{پایان}}
== Specifications (J-10A) ==
[[File:Chengdu J-10.svg|left|300px|An orthographically projected diagram of the Chengdu J-10]]
{{Aircraft specs
|ref={{citation needed|date=September 2019}}
|prime units?=met
<!--
General characteristics
-->
|crew=1<ref name="sinodefense"/>
|length m=۱۶٫۴۳
|length note=
|span m=۹٫۷۵
|span note=
|height m=۵٫۴۳
|height note=
|wing area sqm=۳۳
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=<!--'''root:''' [[NACA airfoil|NACA]]; '''tip:''' [[NACA airfoil|NACA]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |accessdate=16 April 2019}}</ref>-->
|empty weight kg=۹۷۵۰
|empty weight note=<ref name="af-tech">{{cite web |url=http://www.airforce-technology.com/projects/j-10/ |title=J-10 (Jian 10) – Vigorous Dragon Multi-Role Tactical Fighter, China|date=10 February 2008 |publisher=SPG Media Limited |archive-url=https://web.archive.org/web/20070713044152/http://www.airforce-technology.com/projects/j-10/ |archive-date=13 July 2007 |url-status=live}}{{Unreliable source?|reason=domain on WP:BLACKLIST|date=June 2016}}</ref>
|gross weight kg=۱۲۴۰۰
|gross weight note=
|max takeoff weight kg=۱۹۲۷۷
|max takeoff weight note=<ref name="sinodefense"/><ref name="af-tech"/>
|fuel capacity=
|more general=
<!--
Powerplant
-->
|eng1 number=۱
|eng1 name=[[Lyulka AL-31|Saturn-Lyulka AL-31FN]]
|eng1 type=[[afterburning turbofan]] engines
|eng1 kn=۷۹٫۴۳
|eng1 note=(or [[WS-10A]])
|eng1 kn-ab=۱۲۵
<!--
Performance
-->
|max speed kmh=
|max speed note=
|max speed mach=
|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=۳۲۰۰
|range note=<ref name="Archived copy">{{Cite web |url=http://m.online.sh.cn/news/content/2018-12/01/content_9129507.htm |title=Archived copy |access-date=18 April 2019 |archive-url=https://web.archive.org/web/20190418033737/http://m.online.sh.cn/news/content/2018-12/01/content_9129507.htm |archive-date=18 April 2019 |url-status=live}}</ref><ref name="af-tech"/>
|combat range km=۱۲۵۰
|combat range note=<ref name="Archived copy"/><ref name="af-tech"/>
* '''Maximum speed:''' [[Mach number|Mach]]2.2<ref name="Archived copy"/><ref>{{cite report |author=Ministry of Defense of Japan |author-link=Ministry of Defense (Japan) |date=2017 |title=Defense of Japan 2017 |url=http://www.mod.go.jp/e/publ/w_paper/pdf/2017/DOJ2017_1-2-3_web.pdf |page=95 |access-date=29 April 2018 |archive-url=https://web.archive.org/web/20180429221903/http://www.mod.go.jp/e/publ/w_paper/pdf/2017/DOJ2017_1-2-3_web.pdf |archivedate=29 April 2018 |url-status=live}}</ref>
|ferry range km=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=۱۸۰۰۰
|ceiling note=<ref name="af-tech"/>
|g limits={{درشت|+}}۹ {{درشت|–}}3<ref name="af-tech"/>
|roll rate=<!-- aerobatic -->
|climb rate ms=
|climb rate note=
|time to altitude=
|wing loading kg/m2=۳۸۱
|wing loading note=
|fuel consumption kg/km=
|power/mass=
|thrust/weight=1.15 (with [[Saturn AL-31FN3]]); 1.16 (with [[WS-10A]])
|more performance=
* '''Instantaneous Turn Rate:''' 31<sup>+</sup> degrees per second
* '''Roll Rate:''' 300<sup>+</sup> degrees per second
<!--*'''Take-off run:''' {{cvt||m|۰}}
* '''Take-off run to {{cvt|15|m|0}}:''' {{cvt||m|۰}}
* '''Landing run:''' {{cvt||m|۰}}
* '''Landing run from {{cvt|15|m|0}}:''' {{cvt||m|۰}}-->
}}
== پیوند به بیرون ==
{{ویکیانبار-رده|Chengdu J-10}}
{{پانویس|۲}}
{{هواپیما-خرد}}
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