# THK-11

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<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. -->
{{Infobox aircraft
| name                = THK-11
| logo                = 
| logo_size           = 
| image               = File:THK11.jpg
| alt                 = 
| caption             = A replica THK-11 on display at the ''[Ankara Türk Hava Kurumu Müzesi](/source/Ankara_T%C3%BCrk_Hava_Kurumu_M%C3%BCzesi)'' - (Ankara Turkish Aeronautical Museum)
| long_caption        = 
| other_names         = 
| aircraft_type       = Cabin [monoplane](/source/monoplane)
| aim                 = 
| outcome             = 
| related             = 
| national_origin     = Turkey
| manufacturer        = {{lang|tr|[Türk Hava Kurumu](/source/T%C3%BCrk_Hava_Kurumu)}} (THK - Turkish Aeronautical Association)
| design_group        = 
| designer            = 
| builder             = 
| issuer              = 
| status              = Abandoned
| owners              = 
| primary_user        = 
| more_users          = 
| service             = 
| major_applications  = 
| proposals           = 
| prototypes          = 
| number_built        = 1
| construction_number = 
| civil_registration  = 
| military_serial     = 
| radio_code          = 
| requirement         = 
| aircraft_carried    = 
| flights             = 
| total_hours         = 
| total_distance      = 
| construction_date   = 
| introduction        = 
| retired             = 
| first_flight        = 1947
| initiated           = 
| in_service          = 
| last_flight         = 
| expected            = 
| developed_from      = 
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}}

The '''THK 11''' was a 1940s prototype [Turkish](/source/Turkey) four-seat [monoplane](/source/monoplane), designed by [Stanisław Rogalski](/source/Stanis%C5%82aw_Rogalski) and built by {{lang|tr|[Türk Hava Kurumu](/source/T%C3%BCrk_Hava_Kurumu)}} (THK - Turkish Aeronautical Association).<ref name="flight" /><ref name="orbis" />

==Design and development==
The THK-11 was a high-wing twin-boom cantilever cabin monoplane with a {{convert|135|hp|kW|0|abbr=on}} [de Havilland Gipsy Major](/source/de_Havilland_Gipsy_Major) piston engine driving a pusher propeller.<ref name="flight" /> It has a fixed nose-wheel landing gear<ref name="orbis" /> and was first flown in 1947.

==Specifications==
{{Aircraft specs
|ref=Jane's All The World's Aircraft 1951–52,<ref name="jawa51 p191c"/> Jane's All The World's Aircraft 1949–50<ref name=jawa49-50/>
|prime units?=met
<!--
        General characteristics
-->
|crew=2
|capacity=1 passenger
|length m=8.44
|length ft=
|length in=
|length note=
|span m=11.80
|span ft=
|span in=
|span note=
|height m=2.59
|height ft=
|height in=
|height note=
|wing area sqm=18.7
|wing area sqft=
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=828
|empty weight lb=
|empty weight note=
|gross weight kg=1150
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[de Havilland Gipsy Major](/source/de_Havilland_Gipsy_Major)
|eng1 type=four-cylinder air-cooled inverted [in-line engine](/source/Inline_engine_(aeronautics))
|eng1 kw=<!-- prop engines -->
|eng1 hp=135<!-- prop engines -->

|prop blade number=2
|prop name=fixed-pitch pusher propeller
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=
<!--
        Performance
-->
|max speed kmh=201
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=164
|cruise speed mph=
|cruise speed kts=
|cruise speed note=<br/>
* '''Landing speed:''' {{cvt|80|km/h|mph kn}}
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=800
|range miles=
|range nmi=
|range note=in still air
|endurance=<!-- if range unknown -->
|ceiling m=3500
|ceiling ft=
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=
|climb rate ftmin=690
|climb rate note=
|time to altitude=
|wing loading kg/m2=61.5
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass={{cvt|18.7|lb/hp|kg/kW|order=flip}}

|more performance=
}}

==See also==
{{aircontent
<!-- include as many lines are appropriate. additional lines/entries with carriage return. -->
|see also=
* [Twin-boom aircraft](/source/Twin-boom_aircraft)
|related=<!-- related developments -->
|similar aircraft=<!-- similar or comparable aircraft -->
* [SECAN Courlis](/source/SECAN_Courlis)
|lists=
}}

==References==
{{Commons category}}
<references>

<ref name="orbis">{{cite book |title= The [Illustrated Encyclopedia of Aircraft](/source/Illustrated_Encyclopedia_of_Aircraft) (Part Work 1982–1985)|publisher= Orbis Publishing|page=2996}}</ref>
<ref name="flight">{{cite magazine|url=http://www.flightglobal.com/pdfarchive/view/1949/1949%20-%201678.html|magazine=[Flight](/source/Flight_International)|date=29 September 1949|title=Progress in Turkey|volume= LVI|issue= 2127|page=442}}</ref>
<ref name="jawa51 p191c">{{cite book|last=Bridgeman|first=Leonard|title=Jane's All The World's Aircraft 1951–52 |year=1951 |publisher=Sampson Low, Marston & Company, Ltd.|location=London |page=191c}}</ref>
<ref name=jawa49-50>{{cite book|last=Bridgeman|first=Leonard|title=Jane's All The World's Aircraft 1949-50 |year=1949|publisher=Sampson Low, Marston & Company, Ltd.|location=London |pages=183c–184c}}</ref>

</references>

{{THK aircraft}}

Category:1940s Turkish civil utility aircraft
Category:Single-engined pusher aircraft
Category:Turkish Aeronautical Association aircraft
Category:High-wing aircraft
Category:Aircraft first flown in 1947
Category:Twin-boom aircraft

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Adapted from the Wikipedia article [THK-11](https://en.wikipedia.org/wiki/THK-11) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/THK-11?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.
