- Design and development Operational history
- Operators
- Specifications
- See also
- References
- External links
name=Piaggio P.111 | image=Piaggio P.111.jpg | caption= }}{{Infobox Aircraft Type | type=High-altitude research aircraft | national origin=Italy | manufacturer=Piaggio | designer= | first flight=9 April 1941 | introduced=1941 | retired=Early 1943 | status= | primary user=Regia Aeronautica (Italian Royal Air Force) | more users= | produced= | number built=1 | variants with their own articles= }} |
The Piaggio P.111 was an Italian high-altitude research aircraft designed and built by Piaggio for the Regia Aeronautica (Italian Royal Air Force). Design and developmentThe genesis of the P.111 was in 1938, when the Regia Aeronautica awarded a contract to Piaggio to construct the prototype of a three-seat, twin-engine, high-speed, high-altitude bomber with a pressurized cabin. Piaggio constructed a new radial engine especially for the P.111, the {{convert|745|kW|hp|abbr=on|0}} 18-cylinder double-row air-cooled Piaggio P.XII R.C.l00/2v, which was fitted with a two-stage supercharger.[1] While the P.111 prototype was under construction, the Regia Aeronatica decided to use it as a high-altitude research aircraft rather than a bomber prototype.[1] Operational historyThe P.111 first flew on 9 April 1941. Employed in research related to pressurization of the cabin of the Piaggio P.108 heavy bomber, it made 110 test and research flights before being retired and scrapped early in 1943.[1] Operators- {{flag|Kingdom of Italy}}
Specifications{{Aircraft specs |ref=Italian Civil & Military Aircraft 1930–1945[2] |prime units?=met |genhide= |crew=three |capacity= |length m= |length ft=40 |length in=8.125 |length note= |span m= |span ft=56 |span in=9 |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=12 |height in=10 |height note= |wing area sqm= |wing area sqft=430 |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb=11,550 |empty weight note= |gross weight kg= |gross weight lb=16,698 |gross weight note= |max takeoff weight kg= |max takeoff weight lb=16,733 |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number=2 |eng1 name=Piaggio P.XII R.C.l00/2v |eng1 type=18-cyl. air-cooled radial piston engines |eng1 kw= |eng1 hp=1,000 |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= |prop name= |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= |max speed mph=357 |max speed kts= |max speed note= at {{convert|10,000|m|ft|abbr=on|0}} |max speed mach= |cruise speed kmh= |cruise speed mph=279 |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= |range miles=1,031 |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= |ceiling ft=39,360 |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=
|armament=
|guns= |bombs= |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other= |avionics= }}See also{{aircontent |see also= |related= |similar aircraft= |sequence= |lists=- List of aircraft of World War II
}}References1. ^1 2 JOHAN VISSCHEDIJK COLLECTION No. 3993. Piaggio P.111 2. ^{{cite book|last=Thompson|first=Jonathan|title=Italian Civil & Military Aircraft 1930–1945|publisher=Aero Publishers Inc.|location=New York|year=1963|edition=1st|pages=232|isbn=0-8168-6500-0}}
External links{{commons category|Piaggio P.111}}- AR Aircraft Manuals Blueprints Video Publications: Piaggio P.111
{{Piaggio aircraft}} 3 : Italian experimental aircraft 1940–1949|Piaggio aircraft|Aircraft first flown in 1941 |