Editing Avro Vulcan (section)

==Specifications (B.1)==
[[File:Avro Vulcan B Mk 2.svg|thumb|upright=1.35|Vulcan B.2]]

{{Aircraft specs
|ref=Polmar,<ref name = 'polmar264'>Polmar and Bell 2004, p. 264.</ref> Laming<ref name="Laming155-182">Laming 2002, pp. 155, 182.</ref>
|prime units?=kts
<!--
        General characteristics
-->
|crew=5 (pilot, co-pilot, AEO, navigator radar, navigator plotter)<ref group ="nb">Two extra seats could be fitted for crew chiefs, for a total of seven crew.</ref>
|length ft=97
|length in=1
|length note=
|span ft=99
|span in=5
|span note=
|height ft=26
|height in=6
|height note=
|wing area sqft=3554
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' [[NACA airfoil|NACA 0010 mod.]]; '''tip:''' [[NACA airfoil|NACA 0008 mod.]]<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=83573
|empty weight note=equipped and crewed
|gross weight lb=
|gross weight note=
|max takeoff weight lb=170000
|max takeoff weight note=
|fuel capacity={{cvt|9280|impgal|USgal l}}; {{cvt|74240|lb|0}}
|more general=
<!--
        Powerplant
-->
|eng1 number=4
|eng1 name=[[Bristol Olympus Mk.101]]  / Mk.102 / Mk.104
|eng1 type=twin-spool [[turbojet]] engines
|eng1 kw=<!-- prop engines -->
|eng1 hp=<!-- prop engines -->
|eng1 shp=<!-- prop engines -->
|eng1 kn=<!-- jet/rocket engines -->
|eng1 lbf=11000
|eng1 note=
<!--
        Performance
-->
|perfhide=

|max speed kts=561
|max speed note=at altitude
|max speed mach=0.96
|cruise speed kts=493
|cruise speed note= / M0.86 at {{convert|45000|ft|m}}
|stall speed kts=
|stall speed note=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kts=
|minimum control speed note=
|range nmi=2265
|range note=
|combat range nmi=
|combat range note=
|ferry range nmi=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=56000
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin=
|climb rate note=
|time to altitude=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption lb/mi=
|thrust/weight=0.31

|more performance=
<!--
        Armament
-->
|armament= * 21 × 1,000 pounds (454&nbsp;kg) of [[gravity bomb|conventional bombs]]
* 1 × [[Blue Danube (nuclear weapon)|Blue Danube]] nuclear gravity bomb
* 1 × [[Violet Club]] 400&nbsp;kt nuclear gravity bomb
* 1 × U.S. [[Mark 5 nuclear bomb|Mark 5]] nuclear gravity bomb supplied under [[Project E]]
* 1 × [[Yellow Sun (nuclear weapon)|Yellow Sun]] Mk.1 400&nbsp;kt nuclear gravity bomb
* 1 × [[Yellow Sun (nuclear weapon)|Yellow Sun]] Mk.2 1.1&nbsp;Mt thermonuclear gravity bomb
* 1 × [[Red Beard (nuclear weapon)|Red Beard]] nuclear gravity bomb
* 1 × [[WE.177B]] parachute-retarded nuclear gravity bomb<ref name = 'kev65'/>

|avionics=
}}

===Comparison of variants===

{| class="wikitable"
|-
|+ Variants compared<ref>Pilot's Notes AP 4505-C PN</ref><ref>Aircrew Manual AP 101B-1902-15</ref>
|-
! style="width:15%;"|
! style="width:17%;"|B.1
! style="width:17%;"|B.1A
! style="width:17%;"|B.2
! style="width:17%;"|B.2 (MRR)
! style="width:17%;"|K.2
|-
! Wingspan
| colspan="2" style="text-align:center;"| {{convert|99|ft|5|in|m|abbr=on}}
| colspan="3" style="text-align:center;"| {{convert|111|ft|0|in|m|abbr=on}}
|-
! Length
| style="text-align:center;"|{{convert|97|ft|1|in|m|abbr=on}}
| colspan="4" style="text-align:center;"|{{convert|105|ft|6|in|m|abbr=on}}      [{{convert|99|ft|11|in|m|abbr=on}} without probe]
|-
! Height
| colspan="2" style="text-align:center;"| {{convert|26|ft|6|in|m|abbr=on}}
| colspan="3" style="text-align:center;"| {{convert|27|ft|1|in|m|abbr=on}}
|-
! Wing area
| colspan="2" style="text-align:center;"|{{convert|3554|sqft|m2|abbr=on}}<ref name="blackman213">Blackman 2007, p. 213.</ref>
| colspan="3" style="text-align:center;"|{{convert|3964|sqft|m2|abbr=on}}<ref name="blackman213"/>
|-
! Max. takeoff weight
| colspan="2" style="text-align:center;"|{{convert|167000|lb|kg|abbr=on}}<br/>{{convert|185000|lb|kg|abbr=on}} (operational necessity)
| colspan="3" style="text-align:center;"|{{convert|204000|lb|kg|abbr=on}}
|-
! Cruising speed
| colspan="5" style="text-align:center;"|Mach 0.86 [[Machmeter|indicated]]
|-
! Max. speed
| colspan="2" style="text-align:center;"|Mach 0.95 indicated
| style="text-align:center;"|Mach 0.93 indicated<br/>(Mach 0.92 with 301 engines)
| style="text-align:center;"|Mach 0.93<br/>indicated
| style="text-align:center;"| Unknown
|-
! Service ceiling
| colspan="2" style="text-align:center;"|56,000&nbsp;ft<ref name="blackman213"/>
| colspan="3" style="text-align:center;"|45,000&nbsp;ft to 60,000&nbsp;ft<ref group="nb">Depended upon oxygen equipment fitted. No airframe limitation on height.</ref>
|-
! Electrical system
| colspan="2" style="text-align:center;"|112 V [[direct current|DC]]
| colspan="3" style="text-align:center;"|115/200 V [[alternating current|AC]] [[Three-phase electric power|3-phase]] 400 [[Hertz|Hz]]
|-
! Emergency electrical<br/>system
| colspan="2" style="text-align:center;"|Battery
| colspan="3" style="text-align:center;"|[[Ram air turbine]] and [[Auxiliary power unit|Airborne Auxiliary Power Plant]]
|-
! Engines
| style="text-align:center;"|4 × [[Rolls-Royce Olympus|Bristol<br/> Olympus 101, 102 or 104]]
| style="text-align:center;"|4 × Bristol<br/> Olympus 104
| style="text-align:center;"|4 × Bristol Siddeley<br/> Olympus 200-series, 301
| colspan="2" style="text-align:center;"|4 × Bristol Siddeley<br/> Olympus 200-series
|-
! Fuel capacity <br/>(main)
| colspan="2" style="text-align:center;"|{{cvt|9280|impgal|USgal l}} / {{cvt|74240|lb|0}} [[Jet fuel|avtur]])<ref group="nb">At specific gravity of .8 (8lb/gal).</ref>
| colspan="3" style="text-align:center;"|{{cvt|9260|impgal|USgal l}} / {{cvt|74080|lb|0}}
|-
! Fuel capacity <br/>(bomb bay)
| colspan="2" style="text-align:center;"|None
| style="text-align:center;"|{{cvt|0|-|1990|impgal|USgal l}} / {{cvt|0|-|15920|lb|0}}
| style="text-align:center;"|{{cvt|1990|impgal|USgal l}} / {{cvt|15920|lb|0}}<ref group="nb">2 × {{cvt|995|impgal|USgal l}} cylindrical tanks.</ref>
| style="text-align:center;"|{{cvt|2985|impgal|USgal l}} / {{cvt|23880|lb|0}}<ref group="nb">3 × {{cvt|995|impgal|USgal l}} cylindrical tanks.</ref>
|-
! Powered flying controls
| colspan="2" style="text-align:center;"|1 × rudder (duplex), 4 × elevators, 4 × ailerons
| colspan="3" style="text-align:center;"|1 × rudder (duplex), 8 × elevons
|-
! Armament
| colspan="2" style="text-align:center;"|1 × free-fall [[nuclear weapon|nuclear bomb]] ''or''<br/>21 × {{convert|1000|lb|abbr=on}}<br/>conventional bombs
| style="text-align:center;"|1 × [[Blue Steel (missile)|Blue Steel]] missile ''or'' <br/>1 × free-fall [[nuclear weapon|nuclear bomb]] ''or''<br/> 21 × {{convert|1000|lb|abbr=on}}<br/> conventional bombs<br/>
| colspan="2" style="text-align:center;"|None <br/>
|}