IMAM Ro.5

{{Infobox aircraft | name = Ro.5 | logo = | logo_size = | image = Pristanek letala na Mengeškem polju leta 1932.jpg | alt = | caption = | long_caption = | other_names = | aircraft_type = Sport aircraft | aim = | outcome = | related = | national_origin = Italy | manufacturer = IMAM | design_group = | designer = Alessandro Tonini | builder = | issuer = | status = | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = 1929 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }}

The '''IMAM Ro.5''' was a sport aircraft designed by Alessandro Tonini and produced by IMAM in Italy in the late 1920s.<ref name="JEA"> {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |page=768 }}</ref>

==Design and development== The Ro.5 was a conventional, parasol wing monoplane with fixed tailskid undercarriage and two open cockpits in tandem.<ref name="IEA">{{cite book |title=The Illustrated Encyclopedia of Aircraft |publisher=Aerospace Publishing|location=London |page=2193 }}</ref> It proved popular with private owners and flying clubs, and was built in large numbers.<ref name="IEA"/> Some Ro.5s were purchased by the ''Regia Aeronautica'' for use as trainers and liaison aircraft.<ref name="IEA"/> A later version, the '''Ro.5bis''', enclosed the cockpits under a long canopy.<ref name="IEA"/>

==Operators== ;{{flag|Kingdom of Italy}} *Regia Aeronautica ;{{ESP}} *Spanish Air Force

==Specifications (Ro.5) == {{Aircraft specs |ref=Jane's all the World's Aircraft 1928,<ref name=JAWA1928>{{cite book |title=Jane's all the World's Aircraft 1928 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |page=169c}}</ref> The Illustrated Encyclopedia of Aircraft<ref name="IEA"/> |prime units?=met  |crew=2 |length m=6.94 |span m=10 |height m=2.16 |wing area sqm=16 |aspect ratio= |airfoil= |empty weight kg=400 |gross weight kg=680 |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general=  |eng1 number=1 |eng1 name=Walter NZ 85 |eng1 type=7-cyl. air-cooled radial piston engine |eng1 hp=85

|prop blade number=2 |prop name=fixed pitch propeller |prop dia m= |prop dia ft= |prop dia in= |prop dia note=  |max speed kmh=175 |max speed note=to {{cvt|180|km/h|mph+kn}} |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh=65 |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |range km=1000 |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=6.5 hours |ceiling m=4000 |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |wing loading kg/m2=42.5 |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass={{cvt|0.05682|hp/lb|kW/kg|order=flip}} |more performance= }}

==References== {{commons category|IMAM Ro.5}} {{reflist}}

Ro.05 Category:1920s Italian sport aircraft Category:Parasol-wing aircraft Category:Single-engined tractor aircraft Category:Aircraft first flown in 1929