Editing Lockheed Vega (section)

==Specifications (Vega 5C)==
[[File:Lockheed Vega 3-view NACA Aircraft Circular No.61.jpg|thumb|three-view drawing of Vega prototype with original small rudder and uncowled engine.]]
[[File:NASM-A19670093000-NASM2018-10372-000001.jpg|thumb|Vega 5B radial engine and prop]]
{{Aircraft specs
|ref=''Lockheed aircraft since 1913.''<ref>{{cite book|last1=Francillon|first1=Rene J.|title=Lockheed aircraft since 1913|date=1988|publisher=Naval Institute Press|location=Annapolis|isbn=0870218972|pages=67–86|edition=2nd reprint}}</ref>
|prime units?=imp
<!--
        General characteristics
-->
|crew=1
|capacity=6 pax
|length ft=27
|length in=6
|length note=
|span ft=41
|span in=
|span note=
|height ft=8
|height in=6
|height note=
|wing area sqft=275
|wing area note=
|airfoil='''root:''' Clark Y (18%) ; '''tip:''' Clark Y (9.47%)<ref>{{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=2565
|empty weight note=<br>
::::Vega 5C floatplane {{cvt|3153|lb}}
|gross weight lb=4500
|gross weight note=<br>
::::Vega 5C floatplane {{cvt|4880|lb}}
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{cvt|160|USgal|impgal l}}
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Pratt & Whitney R-1340C Wasp]]
|eng1 type=9-cylinder air-cooled radial piston engine
|eng1 hp=450
|eng1 note=
|prop blade number=2
|prop name=fixed-pitch propeller
|prop dia ft= |prop dia in= |prop dia note=
<!--
        Performance
-->
|max speed mph=185
|max speed note=with [[NACA cowling]]<br>
::::Vega 5C floatplane with [[NACA cowling]] {{cvt|175|mph}}
|cruise speed mph=165
|cruise speed note=<br>
::::Vega 5C floatplane with [[NACA cowling]] {{cvt|160|mph}}
|stall speed mph=
|stall speed note=
|never exceed speed mph=
|never exceed speed note=
|range miles=725
|range note=<br/>
::::Vega 5C floatplane {{cvt|620|mi}}
|ferry range miles=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=19000
|ceiling note=<br/>
::::Vega 5C floatplane {{cvt|17000|ft}}
|climb rate ftmin=1300
|climb rate note=<br/>
::::Vega 5C floatplane {{cvt|1100|ft/min|m/s}}
|time to altitude=
|wing loading lb/sqft=16.4
|wing loading note=<br/>
::::Vega 5C floatplane {{cvt|17.7|lb/sqft}}
|fuel consumption lb/mi=
|power/mass={{cvt|0.1|hp/lb}}
::::Vega 5C floatplane {{cvt|0.0926|hp/lb}}

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