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Lockheed Martin F-22 Raptor
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==Specifications (F-22A)== [[File:Lockheed Martin F-22A Raptor 3-view line drawing.jpg|thumb|F-22 Raptor 3-view drawings]] [[File:F22 Raptor info.jpg|thumb|USAF poster of key F-22 features and armament]] [[File:F-22 underside.jpeg|thumb|F-22's underside with main bay doors open]] [[File:Lockheed Martin F-22A Raptor JSOH.jpg|thumb|F-22's diamond-like delta wing planform]] {{Aircraft specs |ref= USAF,<ref name="f22_factsheet"/> manufacturers' data,<ref name="lm_specs">{{cite web |url=http://www.lockheedmartin.com/us/products/f22/f-22-specifications.html |title=F-22 Raptor Specifications |publisher=Lockheed Martin |access-date=21 April 2012 |archive-url=https://web.archive.org/web/20120603072326/http://www.lockheedmartin.com/us/products/f22/f-22-specifications.html |archive-date=3 June 2012 |url-status=live}}</ref><ref>[https://web.archive.org/web/20120708073636/http://www.boeing.com/defense-space/military/f22/f22specs.html "F-22 Technical Specs."] Boeing. Retrieved 16 October 2011.</ref><ref name="combat_radius">{{cite web|url=http://2.bp.blogspot.com/-irwcM2ov73s/Toru4NRprRI/AAAAAAAABm4/PBBm_UVa5Ng/s1600/F-22range.jpeg |title=F-22 Combat Radius |access-date=7 June 2016 |archive-url=https://web.archive.org/web/20161105005403/http://2.bp.blogspot.com/-irwcM2ov73s/Toru4NRprRI/AAAAAAAABm4/PBBm_UVa5Ng/s1600/F-22range.jpeg |archive-date=5 November 2016 |url-status=live}}</ref> ''Aerofax'',<ref>Miller 2005, p. 102.</ref> ''[[Aviation Week]]'',<ref name="avweek_20070107"/><ref name="avweek_20141103">{{Cite magazine |author=Bill Sweetman |url=http://aviationweek.com/defense/j-20-stealth-fighter-design-balances-speed-and-agility |title=J-20 Stealth Fighter Design Balances Speed And Agility |magazine=Aviation Week & Space Technology |publisher=Penton Media |date=3 November 2014 |access-date=8 November 2014 |archive-url=https://web.archive.org/web/20141105012355/http://aviationweek.com/defense/j-20-stealth-fighter-design-balances-speed-and-agility |archive-date=5 November 2014 |url-status=live}}</ref> ''[[Air Forces Monthly]]'',<ref name="AFM"/> and ''[[Journal of Electronic Defense]]''<ref name="fighter_EW_next"/> |prime units?=kts <!-- General characteristics --> |genhide= |crew=1 |length m=18.92 |length ft=62 |length in=1 |span m=13.56 |span ft=44 |span in=6 |height m=5.08 |height ft=16 |height in=8 |wing area sqm=78.04 |wing area sqft=840 |aspect ratio=2.36 |airfoil=[[NACA airfoil|NACA 6 series airfoil]] |empty weight kg=19700 |empty weight lb=43340 |empty weight note= |gross weight kg=29410 |gross weight lb=64840 |gross weight note= |max takeoff weight kg=38000 |max takeoff weight lb=83500 |max takeoff weight note= |fuel capacity={{convert|18000|lb|kg|abbr=on}} internally, or {{convert|26000|lb|kg|abbr=on}} with 2Γ 600 U.S. gal tanks |more general= <!-- Powerplant --> |eng1 number=2 |eng1 name=[[Pratt & Whitney F119]]-PW-100 |eng1 type=augmented [[turbofan]]s |eng1 lbf=26000 |eng1 kn=116 |eng1 lbf-ab=35000 |eng1 kn-ab=156 |more power={{refn|Actual thrust is up to {{cvt|37000|lbf|kN|0}}.<ref>AIR International, July 2015, p. 63.</ref>|group=N}} <!-- Performance --> |perfhide= |max speed mach=2.25, {{convert|1500|mph|kn km/h|0|abbr=on}} at altitude<ref name="AFM"/> **Mach 1.21, {{convert|800|knots|mph km/h|0}} at sea level |cruise speed note=*'''Supercruise:''' Mach 1.76, {{convert|1162|mph|kn km/h|0|abbr=on}} at altitude |range nmi=1600 |range note=or more with 2 external fuel tanks |ferry range nmi=1740 |combat range nmi=460 |combat range note=clean with {{convert|100|nmi|mi km|0|abbr=on}} in supercruise **{{convert|595|nmi|mi km|0|abbr=on}} clean subsonic **{{convert|750|nmi|mi km|0|abbr=on}} with 100 nmi in supercruise with 2Γ 600 U.S. gal tanks{{#tag:ref|860 nmi subsonic with 2Γ 600 U.S. gal tanks. All figures include β6% routing factor, combat and 2Γ GBU-32 + 2Γ AIM-9 + 2Γ AIM-120.|group=N}} |ceiling m= |ceiling ft=65000 |climb rate ms= |climb rate ftmin= |wing loading kg/m2= |wing loading lb/sqft=77.2 |wing loading note= |thrust/weight=1.08 (1.25 with loaded weight and 50% internal fuel) |g limits=+9.0/β3.0 |more performance= <!-- Armament --> |armament= *'''Guns:''' 1Γ [[20 mm caliber|20 mm]] [[M61 Vulcan|M61A2 Vulcan]] [[rotary cannon]], 480 rounds *'''Internal weapons bays:''' **'''Air-to-air mission loadout:''' <!--***6Γ [[AIM-260 JATM]] ''or'' --> ***6Γ [[AIM-120 AMRAAM|AIM-120C/D]] AMRAAM ''or'' ***4Γ AIM-120A/B ***2Γ [[AIM-9 Sidewinder|AIM-9M/X Sidewinder]] **'''Air-to-ground mission loadout:''' ***2Γ {{convert|1000|lb|kg|abbr=on}} [[Joint Direct Attack Munition|JDAM]] and 2Γ AIM-120 ''or'' ***8Γ {{convert|250|lb|kg|abbr=on}} [[GBU-39 Small Diameter Bomb|GBU-39 SDB]]<!--/[[GBU-53/B StormBreaker|GBU-53 StormBreaker]]--> and 2Γ AIM-120 ''or'' ***4Γ 250 lb GBU-39 and 4Γ AIM-120 ***2Γ AIM-9 *'''Hardpoint (external)''': **4Γ under-wing pylon stations can be fitted to carry weapons, each with a capacity of 5,000 lb (2,270 kg) ''or'' 600 U.S. gallon (2,270 L) [[drop tank]]s<ref name="Miller_2005_p94-100">Miller 2005, pp. 94β100.</ref> **4x AIM-120 AMRAAM (external) |avionics= *[[AN/APG-77]] or AN/APG-77(V)1 [[active electronically scanned array|AESA]] radar: {{convert|125|-|150|mi|km}} against {{convert|1|m2|sqft|abbr=on}} targets (estimated range), more than {{convert|250|mi|km}} in narrow beams *AN/AAR-56 [[missile approach warning|Missile Launch Detector]] (MLD) *<!--AN/ASG-XX -->Advanced [[Infrared Search and Track]] (IRST) *AN/ALR-94 [[electronic warfare]] system: {{convert|250|nmi|km}} or more detection range for [[radar warning receiver]] (RWR) *Integrated CNI Avionics including: **Inter/Intra-Flight Datalink (IFDL) **MIDS-JTRS **Link 16/[[JTIDS]] **IFF (Mode 5) **Embedded GPS/INS (EGI) **TACAN **[[HAVE QUICK]]/SATURN **[[SINCGARS]] *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."] {{webarchive|url=https://web.archive.org/web/20110716051703/http://www.sharecast.com/cgi-bin/sharecast/story.cgi?story_id=3361020 |date=16 July 2011}} ''Share cast'', 26 March 2010. Retrieved 26 September 2010.</ref> }}
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