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Macchi C.205 Veltro
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==Specifications (C.205V)== [[File:Abitacolo M.C.205V.jpg|thumb|Cockpit of a C.205]] {{Aircraft specs |ref= ''The Complete Book of Fighters''<ref name="Green 3601">Green 1994, pp. 360-361.</ref> |prime units?= met <!-- General characteristics --> |crew= 1 |length m= 8.85 |span m= 10.58 |height m= 3.04 |wing area sqm= 16.8 |aspect ratio=<!-- sailplanes --> |airfoil='''root:''' [[NACA airfoil|NACA 23018 (modified)]]; '''tip:''' [[NACA airfoil|NACA 23009 (modified)]]<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 kg= 2,581 |gross weight kg= 3,408 |max takeoff weight kg= 3,900 |fuel capacity= |more general= <!-- Powerplant --> |eng1 number= 1 |eng1 name= [[Fiat RA.1050 R.C.58 Tifone]] |eng1 type= V-12 inverted liquid-cooled piston engine |eng1 kw= 1,100 |prop blade number= 3 |prop name= constant-speed propeller |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note= <!-- Performance --> |max speed kmh= 642 |max speed note= at {{cvt|7200|m}} |cruise speed kmh= 400 |stall speed kmh= |never exceed speed kmh= |minimum control speed kmh= |range km=950 |combat range km= |ferry range km= |endurance=<!-- if range unknown --> |ceiling m= 11,500 |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |climb rate ms= |time to altitude=,{{cvt|3000|m}} in two minutes and 40 seconds |wing loading kg/m2= 202.9 |fuel consumption kg/km= |power/mass= |thrust/weight= |more performance= |armament= * '''Guns:''' ** 2 Γ 12.7 mm (.5 in) [[Breda-SAFAT]] machine guns, 400 rpg, in the nose ** 2 Γ 20 mm [[MG 151 cannon]], 250 rpg, in the wings * '''Bombs:''' ** 2 Γ {{convert|160|kg|lb|abbr=on}} |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other= |avionics= }}
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