Editing Bell X-2 (section)

==Specifications (X-2)==
[[File:X-2 3-view.svg|right|300px]]
{{Aircraft specs
|ref=''Concept Aircraft: Prototypes, X-Planes and Experimental Aircraft''<ref>Winchester 2005, p. 35.</ref>
|prime units?=imp
<!--
        General characteristics
-->
|crew=1
|length ft=37
|length in=10
|length note=
|span ft=32
|span in=3
|span note=
|height ft=11
|height in=10
|height note=
|wing area sqft=260
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil= [[NACA airfoil|NACA 2S-(50) (05-50) (05-arc)]]<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=12375
|empty weight note=
|gross weight lb=
|gross weight note=
|max takeoff weight lb=24910
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Curtiss-Wright XLR25]]
|eng1 type=liquid-fuelled rocket engine
|eng1 lbf=15000
|eng1 note=at sea level
<!--
        Performance
-->
|max speed mph=2094
|max speed note=
|max speed mach=3.196
|cruise speed mph=
|cruise speed note=
|stall speed mph=
|stall speed note=
|never exceed speed mph=
|never exceed speed note=
|range miles=
|range note=
|combat range miles=
|combat range note=
|ferry range miles=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=126200
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption lb/mi=
|thrust/weight=

|more performance=<!--<br />
*'''Take-off run:''' {{cvt||ft|0}}
*'''Take-off distance to {{cvt|50|ft|0}}:''' {{cvt||ft|0}}
*'''Landing run:''' {{cvt||ft|0}}
*'''Landing distance from {{cvt|50|ft|0}}:''' {{cvt||ft|0}}-->
|avionics=
}}