- Design
- Specifications
- References
{{short description|1930s Italian aircraft}}name=Ca.146 | image= | caption= }}{{Infobox Aircraft Type | type=Reconnaissance | manufacturer=Caproni | designer= | first flight=1935 | introduced= | retired= | status=prototype only | primary user= | more users= | produced= | number built=1 | variants with their own articles= }} |
The Caproni Ca.146 was a high-wing reconnaissance aircraft built by Caproni in the mid-1930s. DesignThe Ca.146 was a derivative of the Ca.127, and was similar in being a high-wing monoplane. However, the Ca.146 was of all-wood construction and had no armament provisions. The Ca.146 prototype (registration MM.131) flew in 1935 and showed good flight characteristics, but won no orders from the Regia Aeronautica. Specifications{{Aircraft specs |ref=[1] |prime units?=met |genhide= |crew=Two |capacity= |length m=9.54 |length ft= |length in= |length note= |span m=12.60 |span ft= |span in= |span note= |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= |swept ft= |swept in= |swept note= |dia m= |dia ft= |dia in= |dia note= |width m= |width ft= |width in= |width note= |height m= |height ft= |height in= |height note= |wing area sqm=23 |wing area sqft= |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg=1950 |empty weight lb= |empty weight note= |gross weight kg=3305 |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number=1 |eng1 name=Isotta Fraschini Asso XI R.C.40 |eng1 type=V-12 water-cooled piston engine |eng1 kw= |eng1 hp=840 |eng1 shp= |eng1 kn= |eng1 lbf= |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 name= |eng2 type= |eng2 kw= |eng2 hp= |eng2 shp= |eng2 kn= |eng2 lbf= |eng2 note= |eng2 kn-ab= |eng2 lbf-ab= |eng3 number= |eng3 name= |eng3 type= |eng3 kw= |eng3 hp= |eng3 shp= |eng3 kn= |eng3 lbf= |eng3 note= |eng3 kn-ab= |eng3 lbf-ab= |more power= |prop blade number=2 |prop name=fixed pitch wooden propeller or 3-bladedground-adjustable metal propeller |prop dia m= |prop dia ft= |prop dia in= |prop dia note= |rot number= |rot dia m= |rot dia ft= |rot dia in= |rot area sqm= |rot area sqft= |rot area note=
|perfhide= |max speed kmh=420 |max speed mph= |max speed kts= |max speed note= |max speed mach= |cruise speed kmh=380 |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=1000 |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling m=8000 |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |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=
|guns= |bombs= }}
References1. ^{{cite web|url=http://www.airwar.ru/enc/other1/ca146.html |title=Caproni Ca.146 |publisher=Airwar.ru |date= |accessdate=2019-02-04}}
{{Caproni aircraft}} 2 : Caproni aircraft|Aircraft first flown in 1935 |