Editing Sopwith Camel (section)

==Specifications (F.1 Camel)==
[[File:Sopwith F.1 Camel drawing.jpg|thumb|Sopwith F.1 Camel drawing]]
{{Aircraft specs
|ref=Quest for Performance,<ref>Loftin, LK, Jr. [http://www.hq.nasa.gov/pao/History/SP-468/cover.htm "Quest for Performance: The Evolution of Modern Aircraft. NASA SP-468".] ''NASA.'' Retrieved: 22 April 2006.</ref> Profile Publications<ref name = "bruce 12">Bruce 1965, p. 12.</ref>
|prime units?=imp
<!--General characteristics-->
|crew=1
|length ft=18
|length in=9
|span ft=28
|span in=0
|height ft=8
|height in=6
|wing area sqft=231
|aspect ratio=4.11
|airfoil=RAF 16<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=930
|gross weight lb=1453
|max takeoff weight lb=
|fuel capacity=
|more general=
* '''[[Zero-lift drag coefficient]]:''' C<sub>D</sub>0.0378
* '''Frontal area:''' {{convert|8.73|sqft|m2}}
<!--Powerplant-->
|eng1 number=1
|eng1 name=[[Clerget 9B]]
|eng1 type=9-cylinder air-cooled [[rotary engine|rotary]] piston engine
|eng1 hp=130

|prop blade number=2
|prop name=fixed-pitch wooden propeller
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=
<!--Performance-->
|max speed mph=113
|stall speed mph=48
|range miles=300
|combat range miles=
|ferry range miles=
|endurance=<!-- if range unknown -->
|ceiling ft=19000
|climb rate ftmin=1085
|climb rate note=
|time to altitude=
|lift to drag=7.7
|wing loading lb/sqft=6.3
|wing loading note=
|fuel consumption lb/mi=
|power/mass={{cvt|0.09|hp/lb}}
<!--Armament-->
|guns=2 × {{cvt|0.303|in|2}} [[Vickers machine guns]]
|avionics=
}}