மில் வி-12
{|{{Infobox aircraft begin
  |name = வி-12 
  |image = Aeroflot Mil V-12 (Mi-12) Groningen Airport.jpg
  |caption = 1971இல் மில் வி-12 
 }}{{Infobox aircraft type
  |type = கனரக உயர்த்தி உலங்கு வானூர்தி
  |manufacturer = மில் 
  |designer = &lt;!--only appropriate for single designers, not project leaders--&gt;
  |first flight = (27 சூன் 1967 – வெற்றியற்ற பறப்பு) 10 சூலை 1968 – முதலாவது வெற்றிகரமான பறப்பு
  |introduced = &lt;!--date the aircraft entered military or revenue service--&gt;
  |retired = &lt;!--date the aircraft left military or revenue service. if vague or multiples, it probably should be skipped--&gt;
  |status = சோதனை, நீக்கம்
  |primary user = [[சோவியத் ஒன்றியம்]]
  |more users = &lt;!--up to three more. please separate with &lt;br/&gt;.--&gt;
  |produced = &lt;!--years in production, e.g. 1970-1999, if still in active use but no longer built--&gt;
  |number built = 2
  |unit cost = 
  |developed from = 
  |variants with their own articles = &lt;!-- variants OF the topic type --&gt;
 }}
 |}
 '''மில் வி-12''' (''Mil V-12'') என்பது இதுவரை உருவாக்கப்பட்ட உலங்கு வானூர்திகளில் பெரியதாகும்.&lt;ref name=&quot;Gordon 2005&quot;&gt;{{cite book |last=Gordon |first=Yefim |coauthors=Dimitriy and Sergey Komissarov |title=Mil's heavylift helicopters : Mi-6, Mi-10, V-12 and Mi-26  |edition=2nd edition |series=Red Star |volume=22 |year=2005 |publisher=Midland Publishing |location=Hinckley |isbn=1-85780-206-3}}&lt;/ref&gt; 
 
 ==விபரம் (வி-12)==
 {{Aircraft specs
 |ref=Mil's heavylift helicopters : Mi-6, Mi-10, V-12 and Mi-26,&lt;ref name=&quot;Gordon 2005&quot;/&gt; Jane's All The World's Aircraft 1975-76&lt;ref name=&quot;janes&quot;&gt;{{cite book
  | editor = J W R Taylor
  | title = Jane's All The World's Aircraft,1975-76
  | url = https://archive.org/details/janesallworldsai0000unse_o5q7
  | year = 1975
  | publisher = Macdonald &amp; Co.
  | location = London
  | isbn = 0-354-00521-9
 }}&lt;/ref&gt;
 |prime units?=met
 &lt;!--
         General characteristics
 --&gt;
 |genhide=
 
 |crew=6 (விமானி, துணைவிமானி, பறப்பு பொறியியலாளர், மின்சார நிபுணர், வழிகாட்டி, செய்திப் பரிமாற்றம் இயக்குபவர்)
 |capacity=196 passengers&lt;br/&gt;
 ::::normal {{convert|20000|kg|lb|abbr=on}}
 ::::maximum {{convert|40000|kg|lb|abbr=on}}
 |length m=37
 |length ft=
 |length in=
 |length note=
 |span m=67
 |span ft=
 |span in=
 |span note=across rotors
 |upper span m=
 |upper span ft=
 |upper span in=
 |upper span note=
 |mid span m=
 |mid span ft=
 |mid span in=
 |mid span note=
 |lower span m=
 |lower span ft=
 |lower span in=
 |lower span note=
 |swept m=&lt;!-- swing-wings --&gt;
 |swept ft=&lt;!-- swing-wings --&gt;
 |swept in=&lt;!-- swing-wings --&gt;
 |swept note=
 |dia m=&lt;!-- airships etc --&gt;
 |dia ft=&lt;!-- airships etc --&gt;
 |dia in=&lt;!-- airships etc --&gt;
 |dia note=
 |width m=&lt;!-- if applicable --&gt;
 |width ft=&lt;!-- if applicable --&gt;
 |width in=&lt;!-- if applicable --&gt;
 |width note=
 |height m=12.5
 |height ft=
 |height in=
 |height note=
 |wing area sqm=
 |wing area sqft=
 |wing area note=
 |swept area sqm=&lt;!-- swing-wings --&gt;
 |swept area sqft=&lt;!-- swing-wings --&gt;
 |swept area note=
 |volume m3=&lt;!-- lighter-than-air --&gt;
 |volume ft3=&lt;!-- lighter-than-air --&gt;
 |volume note=
 |aspect ratio=&lt;!-- sailplanes --&gt;
 |airfoil=
 |empty weight kg=69100
 |empty weight lb=
 |empty weight note=
 |gross weight kg=97000
 |gross weight lb=
 |gross weight note=
 |max takeoff weight kg=105000
 |max takeoff weight lb=
 |max takeoff weight note=
 |fuel capacity=
 |lift kg=&lt;!-- lighter-than-air --&gt;
 |lift lb=&lt;!-- lighter-than-air --&gt;
 |lift note=
 |more general=&lt;br/&gt;
 *'''Freight compartment:''' 28.15×4.4×4.4 மி (92.4×14×14 அடி)
 &lt;!--
         Powerplant
 --&gt;
 |eng1 number=4
 |eng1 name=[[Soloviev D-25]]VF
 |eng1 type=turboshaft engines
 |eng1 kw=&lt;!-- prop engines --&gt;
 |eng1 hp=&lt;!-- prop engines --&gt;
 |eng1 shp=6500
 |eng1 kn=&lt;!-- jet/rocket engines --&gt;
 |eng1 lbf=&lt;!-- jet/rocket engines --&gt;
 |eng1 note=
 |power original=
 |thrust original=
 |eng1 kn-ab=&lt;!-- afterburners --&gt;
 |eng1 lbf-ab=&lt;!-- afterburners --&gt;
 
 |eng2 number=
 |eng2 name=
 |eng2 type=
 |eng2 kw=&lt;!-- prop engines --&gt;
 |eng2 hp=&lt;!-- prop engines --&gt;
 |eng2 shp=&lt;!-- prop engines --&gt;
 |eng2 kn=&lt;!-- jet/rocket engines --&gt;
 |eng2 lbf=&lt;!-- jet/rocket engines --&gt;
 |eng2 note=
 |eng2 kn-ab=&lt;!-- afterburners --&gt;
 |eng2 lbf-ab=&lt;!-- afterburners --&gt;
 
 |eng3 number=
 |eng3 name=
 |eng3 type=
 |eng3 kw=&lt;!-- prop engines --&gt;
 |eng3 hp=&lt;!-- prop engines --&gt;
 |eng3 shp=&lt;!-- prop engines --&gt;
 |eng3 kn=&lt;!-- jet/rocket engines --&gt;
 |eng3 lbf=&lt;!-- jet/rocket engines --&gt;
 |eng3 note=
 |eng3 kn-ab=&lt;!-- afterburners --&gt;
 |eng3 lbf-ab=&lt;!-- afterburners --&gt;
 |more power=
 
 |prop blade number=&lt;!-- propeller aircraft --&gt;
 |prop name=
 |prop dia m=&lt;!-- propeller aircraft --&gt;
 |prop dia ft=&lt;!-- propeller aircraft --&gt;
 |prop dia in=&lt;!-- propeller aircraft --&gt;
 |prop dia note=
 
 |rot number=2
 |rot dia m=35
 |rot dia ft=&lt;!-- helicopters --&gt;
 |rot dia in=&lt;!-- helicopters --&gt;
 |rot area sqm=&lt;!-- helicopters --&gt;
 |rot area sqft=&lt;!-- helicopters --&gt;
 |rot area note=5-bladed rotors located transversely
 &lt;!--
         Performance
 --&gt;
 |perfhide=
 
 |max speed kmh=260
 |max speed mph=
 |max speed kts=
 |max speed note=
 |max speed mach=&lt;!-- supersonic aircraft --&gt;
 |cruise speed kmh=240
 |cruise speed mph=
 |cruise speed kts=
 |cruise speed note=
 |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=
 |minimum control speed kmh=
 |minimum control speed mph=
 |minimum control speed kts=
 |minimum control speed note=
 |range km=500
 |range miles=
 |range nmi=
 |range note=
 |combat range km=
 |combat range miles=
 |combat range nmi=
 |combat range note=
 |ferry range km=1000
 |ferry range miles=
 |ferry range nmi=
 |ferry range note=
 |endurance=&lt;!-- if range unknown --&gt;
 |ceiling m=3500
 |ceiling ft=
 |ceiling note=
 |g limits=&lt;!-- aerobatic --&gt;
 |roll rate=&lt;!-- aerobatic --&gt;
 |glide ratio=&lt;!-- sailplanes --&gt;
 |climb rate ms=
 |climb rate ftmin=
 |climb rate note=
 |time to altitude=
 |sink rate ms=&lt;!-- sailplanes --&gt;
 |sink rate ftmin=&lt;!-- sailplanes --&gt;
 |sink rate note=
 |lift to drag=
 |wing loading kg/m2=
 |wing loading lb/sqft=
 |wing loading note=
 |disk loading kg/m2=
 |disk loading lb/sqft=
 |disk loading note=
 |fuel consumption kg/km=
 |fuel consumption lb/mi=
 |power/mass=
 |thrust/weight=
 
 |more performance=&lt;br/&gt;
 *'''Hovering ceiling in ground effect:''' {{convert|600|m|ft|abbr=on}}
 *'''Hovering ceiling out of ground effect:''' {{convert|10|m|ft|abbr=on}}
 &lt;!--
         Armament
 --&gt;
 |armament=&lt;!-- add bulletted list here or if you want to use the following 
 specific parameters, remove this parameter--&gt;
 |guns= 
 |bombs= 
 |rockets= 
 |missiles= 
 |hardpoints=
 |hardpoint capacity=
 |hardpoint rockets=
 |hardpoint missiles=
 |hardpoint bombs=
 |hardpoint other=
 
 |avionics=
 }}
 
 ==குறிப்புக்கள்==
 {{reflist|2}}
 
 ==வெளி இணைப்புக்கள்==
 {{commons category|Mil V-12}}
 * [http://www.aviation.ru/Mi/#12 Mil V-12 data and photos] {{Webarchive|url=https://web.archive.org/web/20060514065019/http://www.aviation.ru/Mi/#12 |date=2006-05-14 }} at [[aviation.ru]]
 * [http://www.avia-dejavu.net/photo%20CCCP-21142.htm about Mil V-12 CCCP-21142] at [[Avia-dejavu.net]]
 * [http://www.airliners.net/search/photo.search?aircraft_genericsearch=&amp;airlinesearch=&amp;countrysearch=&amp;specialsearch=&amp;daterange=&amp;keywords=Mil+Mi-12&amp;range=&amp;sort_order=&amp;page_limit=15&amp;thumbnails=&amp;calccount=1240021&amp;truecount=false&amp;engine_version=6.0 Mil Mi-12 'Homer'] on [[Airliners.net]]
 * [http://www.youtube.com/watch?v=kKsWTdjnXiw Mil-12 video in English]