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词条 THK-5
释义

  1. Variants

  2. Specifications (THK-5A)

  3. References

name=THK-5, THK-10 image= caption=

}}{{Infobox Aircraft Type

type=Air ambulance and light transport national origin=Turkey manufacturer=Turk Hava Kurumu Ucak Fabrikasi (THK) designer= first flight=1945 introduced= retired= status= primary user= number built=13 developed from= variants with their own articles=
}}

The THK-5 was a twin-engine aircraft developed bt in Turkey in 1945 as an air ambulance.[1][2] It was a conventional, low-wing cantilever monoplane of wooden construction throughout. The main units of the tailwheel undercarriage retracted into the wing-mounted engine nacelles and the THK-5 could carry two stretcher cases plus a medical attendant. This was followed in production by a six-seat utility transport version designated THK-5A[2] and three examples of an improved version of the 5A designated THK-10.[3] A single example of the type was exported, sold to Denmark.

When THK was taken over by MKEK, this was one of the designs selected for further work. However, although the designation MKEK-5 was allocated,[1] nothing further came of this.[3]

Variants

THK-5
Air ambulance aircraft, carrying two stretcher cases plus a medical attendant.
THK-5A
6-seat utility transport
THK-10
An improved version of the THK-5A; three built.
MKEK-5
The THK-5, THK-5A and THK-10 re-designated after THK was taken over by Makina ve Kimya Endüstrisi Kurumu (MKEK), but no further development took place.

Specifications (THK-5A)

{{Aircraft specs
|ref=Jane's all the World's Aircraft 1949-50[4]
|prime units?=met


|crew=2
|capacity=4 pax
|length m=10
|span m=14.64
|upper span m=
|mid span m=
|lower span m=
|width m=
|height m=3.1
|wing area sqm=
|aspect ratio=
|airfoil=
|empty weight kg=1355
|gross weight kg=1930
|max takeoff weight kg=
|fuel capacity=
|more general=


|eng1 number=2
|eng1 name=de Havilland Gipsy Major
|eng1 type=4-cylinder inverted air-cooled in-line piston engines
|eng1 hp=135
|prop blade number=2
|prop name=wooden fixed-pitch propellers
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|max speed kmh=220
|max speed mach=
|cruise speed kmh=200
|cruise speed note=

  • Landing speed: {{cvt|120|km/h|mph kn}}

|stall speed kmh=
|never exceed speed kmh=
|minimum control speed kmh=
|range km=
|combat range km=
|ferry range km=
|endurance=
|ceiling m=4000
|g limits=
|roll rate=
|climb rate ms=3.5
|time to altitude=
|wing loading kg/m2=64
|fuel consumption kg/km=
|power/mass={{cvt|16.28|lb/hp|kg/kW|order=flip}}
|thrust/weight=
|more performance=
}}

References

1. ^{{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |page=683 }}
2. ^{{cite journal |title=The Turkish Air League |journal=Flight |date=24 March 1949|pages =350–52 |url=http://www.flightglobal.com/pdfarchive/view/1949/1949%20-%200546.html |accessdate=2008-10-27 |volume=Vol. LV |issue= No. 2100 |page=}}
3. ^{{cite book |last= Deniz |first= Tuncay |title=Turkish Aircraft Production |year=2004 |publisher=Levent Başara |location=Munich |pages= }}
4. ^{{cite book |title=Jane's all the World's Aircraft 1949-50 |edition= |editor1-last=Bridgman |editor1-first=Leonard |year=1949 |publisher=Sampson Low, Marston & Co |location=London |page=184c}}
{{THK aircraft}}{{MKEK aircraft}}

5 : Turkish civil utility aircraft 1940–1949|Twin-engined tractor aircraft|Low-wing aircraft|THK aircraft|Aircraft first flown in 1945

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