எப்-22: திருத்தங்களுக்கு இடையிலான வேறுபாடு
உள்ளடக்கம் நீக்கப்பட்டது உள்ளடக்கம் சேர்க்கப்பட்டது
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வரிசை 25:
==விவரக்கூற்று==
[[File:F22a3view.png|right|300px|Orthographically projected diagram of the F-22A]]
{{aircraft specifications
<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]].
Please answer the following questions: -->
|plane or copter=plane
|jet or prop?=jet
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses).
If an item doesn't apply, like capacity, leave it blank. For additional lines, end your alt units with a right parenthesis ")" and start a new, fully-formatted line beginning with an asterisk "*"
-->
|ref=USAF,<ref name="F-22_factsheet"/> F-22 Raptor Team web site,<ref name="flt_test">[http://www.f22-raptor.com/technology/data.html "Flight Test Data."] ''F-22 Raptor team''. Retrieved: 18 April 2006.</ref> ''Manufacturers' data'', <ref name="lm_specs">[http://www.lockheedmartin.com/us/products/f22/f-22-specifications.html "F-22 Raptor Specifications."] ''Lockheed Martin''. Retrieved: 21 April 2012.</ref><ref>[http://www.boeing.com/defense-space/military/f22/f22specs.html "F-22 Technical Specs."] ''Boeing''. Retrieved: 16 October 2011.</ref> ''[[Aviation Week]]'',<ref name="avweek_20070107_ul"/> and ''[[Journal of Electronic Defense]]'',<ref name="fighter_EW_next"/>
<!--
General characteristics -->
|crew=1
|length main=62 ft 1 in
|length alt=18.90 m
|span main=44 ft 6 in
|span alt=13.56 m
|height main=16 ft 8 in
|height alt=5.08 m
|area main=840 ft²
|area alt=78.04 m²
|airfoil=[[NACA airfoil|NACA 64A?05.92]] root, NACA 64A?04.29 tip
|empty weight main=43,430 [[pound (mass)|lb]]
|empty weight alt=19,700 kg<ref name="F-22_factsheet"/><ref name="lm_specs"/>
|loaded weight main=64,460 lb
|loaded weight alt=29,300 kg{{#tag:ref| empty weight+ 8,200 kg(fuel) + 1,142 kg (6 AMRAAM + 2 AIM-9X) + 292 kg (munition for the canon)<ref>[http://www.lockheedmartin.com/products/f22/f-22-specifications.html "F-22 Specifications."]{{dead link|date=January 2012}} ''Lockheed Martin''. Retrieved: 26 September 2010.</ref>|group=N}}
|max takeoff weight main=83,500 lb
|max takeoff weight alt=38,000 kg
|more general='''Fuel capacity:''' 18,000 lb (8,200 kg) internally,<ref name="F-22_factsheet"/><ref name="lm_specs"/> or 26,000 lb (11,900 kg) with two external fuel tanks<ref name="F-22_factsheet"/><ref name="lm_specs"/>
<!--
Powerplant -->
|engine (jet)=[[Pratt & Whitney F119|Pratt & Whitney F119-PW-100]]
|type of jet=Pitch Thrust vectoring [[turbofan]]s
|number of jets=2
|thrust main=23,500 lb<ref name=Miller_p108>Miller 2005, p. 108.</ref>
|thrust alt=104 kN
|afterburning thrust main= 35,000+ lb<ref name="F-22_factsheet"/><ref name=Miller_p108/>
|afterburning thrust alt= 156+ kN
<!--
Performance -->
|max speed main=<br>
**'''At altitude:''' [[Mach number|Mach]] 2.25 (1,500 mph, 2,410 km/h) [estimated]<ref name="AFM"/>
**'''[[Supercruise]]:''' Mach 1.82 (1,220 mph, 1,963 km/h)<ref name="AFM"/>
|cruise speed main=
|cruise speed alt=
|cruise speed more=
|ferry range main=2,000 mi
|ferry range alt=1,738 [[nautical mile|nmi]], 3,219 km
|range main= >1,600 nmi
|range alt= 1,840 mi, 2,960 km
|range more=with 2 external fuel tanks
|combat radius main=410 nmi (with 100 nmi in supercruise) <ref name="flt_test"/>
|combat radius alt=471 mi, 759 km
|combat radius more=
|ceiling main=65,000 ft
|ceiling alt=19,812 m
|climb rate main=
|climb rate alt=
|loading main=77 lb/ft²
|loading alt=375 kg/m²
|thrust/weight=1.09 <!-- Thrust/loaded weight per [[WP:Air/PC]], e.g. 70,000 lb/64,460 lb = 1.09 --> (1.26 with loaded weight & 50% fuel)
|more performance= *'''Maximum design ''g''-load:''' -3.0/+9.0 g<ref name="AFM"/>
<!--
Armament & Avionics -->
[[File:F22 Raptor info.jpg|thumb|300px|USAF poster overview of key features and armament]]
|armament=
*'''Guns:''' 1× [[20 mm caliber|20 mm (0.787 in)]] [[M61 Vulcan|M61A2 Vulcan]] [[Gatling gun#M61 Vulcan, Minigun, and other designs|6-barreled gatling cannon]] in starboard wing root, 480 rounds
*'''Air to air loadout:'''
**6× [[AIM-120 AMRAAM]]
**2× [[AIM-9 Sidewinder]]
*'''Air to ground loadout:'''
**2× [[AIM-120 AMRAAM]] ''and''
**2× [[AIM-9 Sidewinder]] ''for [[Air to air combat|self-protection]], and one of the following:''
***2× {{convert|1000|lb|abbr=on}} [[Joint Direct Attack Munition|JDAM]] ''or''
***8× {{convert|250|lb|abbr=on}} [[GBU-39 Small Diameter Bomb]]s
*'''[[Hardpoint]]s:''' 4× under-wing pylon stations can be fitted to carry 600 US [[gallon]] [[drop tank]]s ''or'' weapons, each with a capacity of 5,000 lb (2,268 kg).<ref name=Miller_2005_p94-100>Miller 2005, pp. 94–100.</ref>
|avionics=
*'''RWR ([[Radar warning receiver]]):''' 250 [[nautical mile|nmi]] (463 km) or more<ref name="fighter_EW_next"/>
*'''[[Radar]]:''' 125–150 miles (200–240 km) against {{convert|1|m2|sqft|abbr=on}} targets (estimated range)<ref name="avweek_20070107_ul"/>
*[[Chemring]] MJU-39/40 flares for protection against IR missiles.<ref>Wild, Lee. [http://www.sharecast.com/cgi-bin/sharecast/story.cgi?story_id=3361020 "US quick to return for Chemring's flares."] ''Sharecast.com,'' 26 March 2010. Retrieved: 26 September 2010.</ref>
}}
==குறிப்புகள்==
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