Editing Concorde (section)

==Specifications==
[[File:Concorde v1.0.png|thumb|Other line drawings of Concorde]]
[[File:Concorde G-BOAC.png|thumb|Concorde G-BOAC]]

{{Aircraft specs
|ref= ''The Wall Street Journal'',<ref name="fliengi">{{cite news |url=https://www.wsj.com/articles/SB106504293992222300?mod=googlewsj |title=Final Boarding Call: As Concorde Departs, so do 3-Man Crews: In New Cockpits, Engineers are seen as Extra Baggage |work=The Wall Street Journal |first=Danial |last=Michaels |date=2 October 2003 |access-date=3 August 2017 |archive-date=5 October 2017 |archive-url=https://web.archive.org/web/20171005000348/https://www.wsj.com/articles/SB106504293992222300?mod=googlewsj |url-status=live}}</ref> ''The Concorde Story'',{{sfn|Kelly|2005|p=52}} ''The International Directory of Civil Aircraft'',{{sfn|Frawley|2003|p=14}}
''Aérospatiale/BAC Concorde 1969 onwards (all models)''<ref>{{cite book 
|last1=Leney 
|first1=David
|last2=Macdonald <!-- Not a mistake: it's consistently printed as Macdonald in the book, not MacDonald -->
|first2=David 
|title=Aérospatiale/BAC Concorde 1969 onwards (all models)
|publisher=Haynes Publishing
|location=Sparkford, Somerset
|date= 2020
|isbn=978-1-84425-818-5
}}</ref>
|prime units?= imp
<!--   General characteristics
-->
|genhide=

|crew= 3 (2 pilots and 1 [[flight engineer]])
|capacity= 92–120 passengers <br/>(128 in high-density layout)
|length m = 61.66
|length note=
|span m= 25.6
|span note=
|height m= 12.2
|height note=
|wing area sqm= 358.25
|wing area note=
|airfoil=
|empty weight kg= 78,700
|gross weight kg= 111,130
|gross weight note=
|max takeoff weight kg= 185,070
|fuel capacity= {{convert|210940|lb|kg|abbr=on}}; {{cvt|119600|L}}
|more general=
* '''Fuselage internal length:''' {{convert|129|ft|0|in|m|abbr=on}}
* '''Fuselage width:''' maximum of {{convert|9|ft|5|in|m|abbr=on}} external, {{convert|8|ft|7|in|m|abbr=on}} internal
* '''Fuselage height:''' maximum of {{convert|10|ft|10|in|m |abbr=on}} external, {{convert|6|ft|5|in|m|abbr=on}} internal
* '''Maximum taxiing weight:''' {{convert|412000|lb|kg|abbr=on}}
<!--   Powerplant
-->
|eng1 number= 4
|eng1 name= [[Rolls-Royce/Snecma Olympus 593]] Mk 610
|eng1 type= [[turbojet]]s with [[reheat]]
|eng1 lbf=31000
|eng1 kn= 140
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab= 169
|eng1 lbf-ab= 38,050
<!--   Performance
-->
|perfhide=

|max speed kmh= 2,179
|max speed note=
|max speed mach= 2.04 (temperature limited) <!-- temperature limited is relevant, since most aircraft are limited in speed by power or aerodynamics: Concorde is unusual in that is has the power and aerodynamics to go faster -->
|cruise speed kmh= 2,158
|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= 7,222.8
|range note=
|endurance=<!-- if range unknown -->
|ceiling m= 18,300
|ceiling note=
|climb rate ms= 17–25
|climb rate note= at sea level<ref>{{cite journal |title=First Concorde Supersonic Transport Flies |date=17 March 1969 |pages=284 |url=http://aviationweek.com/site-files/aviationweek.com/files/uploads/2015/02/1969-%20First%20Concorde%20Flight%20%281%20of%202%29.pdf |access-date=27 January 2019 |journal= Aviation Week & Space Technology |archive-date=20 December 2016 |archive-url=https://web.archive.org/web/20161220202734/http://aviationweek.com/site-files/aviationweek.com/files/uploads/2015/02/1969-%20First%20Concorde%20Flight%20%281%20of%202%29.pdf |url-status=live}}</ref><ref>{{cite web |title=Concorde Airframe |url=https://www.heritageconcorde.com/airframe-performance |website=Heritage Concorde |access-date=27 January 2019 |language=en |archive-date=28 January 2019 |archive-url=https://web.archive.org/web/20190128030455/https://www.heritageconcorde.com/airframe-performance |url-status=live}}</ref>
|time to altitude=
|lift to drag= ''Low speed–'' 3.94; ''Approach–'' 4.35; ''250 kn, 10,000 ft–'' 9.27; ''Mach 0.94–'' 11.47, ''Mach 2.04–'' 7.14
|wing loading kg/m2=
|wing loading note=
|disk loading kg/m2=
|disk loading note=
|fuel consumption kg/km= 13.2
|power/mass=
|thrust/weight= 0.373
|more performance=
* '''Maximum [[Heat shield|nose tip temperature]]:''' {{convert|127|°C|°F+K|abbr=on|sigfig=2}}
* '''[[Runway]] requirement''' (with maximum load): {{convert|3600|m|ft|abbr=on}}<ref>{{cite web|url=http://www.asiatraveltips.com/travelnews2001/17October2001AirFrance.htm|title=Extremely Comprehensive Concorde Relaunch Kit from Air France|date=17 October 2001|website=Travel News Asia|access-date=13 January 2014|archive-date=13 January 2014|archive-url=https://web.archive.org/web/20140113203252/http://www.asiatraveltips.com/travelnews2001/17October2001AirFrance.htm|url-status=live}}</ref>

|avionics= 
* [[Rolls-Royce/Snecma Olympus 593#Intake|Digital Air Intake Control Units]]
* Fly by wire flight controls
* Analogue electronic engine controls
* Triple [[inertial navigation unit]]s, one per flight crew
* Dual [[VHF omnidirectional range]] instruments
* Dual [[automatic direction finder]] instruments
* Dual [[distance measuring equipment]] instruments
* Triple [[Delco Carousel]] Inertial Navigation Units<ref>{{cite web |url=https://www.heritageconcorde.com/pilots-instruments |title=Concorde Pilots Instruments |website=Heritage Concorde |access-date=22 January 2025}}</ref>
* Dual [[instrument landing system]]s
* Automatic flight control system with dual [[autopilot]]s, [[autothrottle]]s, and [[Flight director (aeronautics)|flight directors]]: full autoland capability with visibility limits {{convert|250|m|ft|abbr=on}} horizontally, {{convert|15|ft|m|abbr=on}} decision height
* [[Ekco]] E390/564 weather radar<ref>{{cite periodical|title=Concorde|periodical=Interavia|volume=24|date=1969|page=397}}</ref>
* Radio altimeters <!-- Radio altimeter is the precise term used in the Haynes book -->
}}