Editing Avro Canada CF-105 Arrow (section)

==Specifications (Arrow Mk 1)==
[[File:Avro Arrow 3-view.jpg|300px|right|Avro CF-105 Arrow 3-view]]
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|image1=[https://www.flickr.com/photos/flightglobal/15028976973/ Cutaway of the Avro CF-105 Arrow] by [[Flight Global]].
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{{Aircraft specs
| ref = ''The Great Book of Fighters'',<ref>Green, William and Gordon Swanborough. ''The Great Book of Fighters''. St. Paul, Minnesota: MBI Publishing, 2001. {{ISBN|0-7603-1194-3}}.</ref> ''The Canadian Approach to All-Weather Interceptor Development'',<ref name="Floyd 1958"/> ''Avro Arrow: The Story of the Avro Arrow from its Evolution to its Extinction''<ref name = 'page116'/>
| prime units? = kts<!--        General characteristics-->
| crew = 2
| length ft = 77
| length in = 9
| length note = 
| span ft = 50
| span in = 
| span note = 
| height ft = 21
| height in = 2
| height note = 
| wing area sqft = 1225
| wing area note = 
| aspect ratio = <!-- sailplanes -->
| airfoil = '''root:'''  [[NACA airfoil|NACA 0003.5 (modified)]]; '''tip:''' [[NACA airfoil|NACA 0003.8 (modified)]]<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 |access-date=16 April 2019}}</ref>
| empty weight lb = 49040
| empty weight note = 
| gross weight kg = 
| gross weight lb = 56920
| gross weight note = 
| max takeoff weight kg = 
| max takeoff weight lb = 68605
| max takeoff weight note = 
| fuel capacity = 
| more general = <!--
        Powerplant
-->
| eng1 number = 2
| eng1 name = [[Pratt & Whitney J75-P-3]]
| eng1 type = [[afterburning turbojet]] engines
| eng1 lbf = 16500
| eng1 note = {{#tag:ref|A wide variety of sources confuse the J75 used in the Arrow with its smaller cousin, the [[Pratt & Whitney J57]]. The J-57 produced about {{cvt|12,500|lbf|kN}} dry and {{cvt|18,500|lbf|kN}} in afterburner.|group=Note}}
| eng1 lbf-ab = 23500
<!--
        Performance
-->| max speed kts = 1136
| max speed note = at {{cvt|50000|ft}} max. recorded speed (Mach 2+ potential)<ref name = 'page116'>Page et al. 2004, p.&nbsp;116.</ref>
| max speed mach = 1.98
| cruise speed kts = 527
| cruise speed note = / M0.91 at {{cvt|36000|ft}}
| stall speed kts = 
| stall speed note = 
| never exceed speed kts = 
| never exceed speed note = 
| minimum control speed kts = 
| minimum control speed note = 
| range nmi = 
| range note = 
| combat range nmi = 261
| combat range note = (combat radius)
| ferry range nmi = 
| ferry range note = 
| endurance = <!-- if range unknown -->
| ceiling ft = 53000
| ceiling note = 
| g limits = <!-- aerobatic -->
| roll rate = <!-- aerobatic -->
| glide ratio = <!-- sailplanes -->
| climb rate ftmin = 
| climb rate note = 
| time to altitude = 
| wing loading lb/sqft = 46.5
| wing loading note = 
| fuel consumption lb/mi = 
| power/mass = 
| thrust/weight = 0.825 at loaded weight
| more performance = <!--
        Armament
-->
| missiles = * 2× [[AIR-2 Genie|AIR-2A Genie]] unguided nuclear rockets<ref>{{cite web| url=https://documents.techno-science.ca/documents/CASM-Aircrafthistories-AvroCanadaCF-105Arrownose.pdf| title=Avro Canada CF-105 Arrow RCAF Serial 25206 (Nose Section & Components)| first=T.F.J.| last=Leversedge| publisher=Canada Aviation and Space Museum| page=31| access-date=14 May 2017| archive-date=2 August 2018| archive-url=https://web.archive.org/web/20180802101743/https://documents.techno-science.ca/documents/CASM-Aircrafthistories-AvroCanadaCF-105Arrownose.pdf| url-status=dead}}</ref>
::''or''
* Up to 4× [[Canadair Velvet Glove]] (cancelled 1956) or 8x [[AIM-4 Falcon]] ''or'' 3 [[AIM-7 Sparrow II]] 2D active guidance missiles (cancelled)
| avionics = * Hughes MX-1179 fire control system
}}