IMAM Ro.5: Difference between revisions
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{|{{Infobox Aircraft Begin |
{|{{Infobox Aircraft Begin |
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| name= |
| name=Ro.5 |
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| image=Pristanek letala na Mengeškem polju leta 1932.jpg |
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| image= |
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| caption= |
| caption= |
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}}{{Infobox Aircraft Type |
}}{{Infobox Aircraft Type |
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| type= |
| type=Sport aircraft |
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| national origin= |
| national origin=Italy |
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| manufacturer= |
| manufacturer=[[IMAM]] |
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| designer= |
| designer=[[Alessandro Tonini]] |
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| first flight= |
| first flight=1929 |
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| introduced= |
| introduced= |
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| retired= |
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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> |
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<!-- ==Development== --> |
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==Design and development== |
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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"/> |
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==Operators== |
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;{{flag|Kingdom of Italy}} |
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*[[Regia Aeronautica]] |
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;{{ESP}} |
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*[[Spanish Air Force]] |
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==Specifications (Ro.5) == |
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{{Aircraft specs |
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|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"/> |
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==Specifications (variant) == |
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|prime units?=met |
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{{aerospecs |
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General characteristics |
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|met or eng?=<!-- eng for US/UK aircraft, met for all others. You MUST include one or the other here, or no specifications will show --> |
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|crew= |
|crew=2 |
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|length m=6.94 |
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|capacity= |
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|span m=10 |
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|height m=2.16 |
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|length ft= |
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|wing area sqm=16 |
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|length in= |
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|span m= |
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|span ft= |
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|span in= |
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|swept m=<!-- swing-wings --> |
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|swept ft=<!-- swing-wings --> |
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|swept in=<!-- swing-wings --> |
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|rot number=<!-- helicopters --> |
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|rot dia m=<!-- helicopters --> |
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|rot dia ft=<!-- helicopters --> |
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|rot dia in=<!-- helicopters --> |
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|dia m=<!-- airships etc --> |
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|dia ft=<!-- airships etc --> |
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|dia in=<!-- airships etc --> |
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|width m=<!-- if applicable --> |
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|width ft=<!-- if applicable --> |
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|width in=<!-- if applicable --> |
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|height m= |
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|height ft= |
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|height in= |
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|wing area sqm= |
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|wing area sqft= |
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|swept area sqm=<!-- swing-wings --> |
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|swept area sqft=<!-- swing-wings --> |
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|rot area sqm=<!-- helicopters --> |
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|rot area sqft=<!-- helicopters --> |
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|volume m3=<!-- lighter-than-air --> |
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|volume ft3=<!-- lighter-than-air --> |
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|aspect ratio=<!-- sailplanes --> |
|aspect ratio=<!-- sailplanes --> |
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|airfoil= |
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|wing profile=<!-- sailplanes --> |
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|empty weight kg= |
|empty weight kg=400 |
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|gross weight kg=680 |
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|max takeoff weight kg= |
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|max takeoff weight lb= |
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|max takeoff weight note= |
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|lift kg=<!-- lighter-than-air --> |
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|fuel capacity= |
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|lift lb=<!-- lighter-than-air --> |
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|more general= |
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|eng1 number= |
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Powerplant |
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|eng1 type= |
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|eng1 kw=<!-- prop engines --> |
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|eng1 |
|eng1 number=1 |
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|eng1 |
|eng1 name=[[Walter NZ 85]] |
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|eng1 |
|eng1 type=7-cyl. air-cooled radial piston engine |
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|eng1 |
|eng1 hp=85 |
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|eng1 lbf-ab=<!-- afterburners --> |
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|eng2 number= |
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|eng2 type= |
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|eng2 kw=<!-- prop engines --> |
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|eng2 hp=<!-- prop engines --> |
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|eng2 kn=<!-- jet/rocket engines --> |
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|eng2 lbf=<!-- jet/rocket engines --> |
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|eng2 kn-ab=<!-- afterburners --> |
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|eng2 lbf-ab=<!-- afterburners --> |
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|prop blade number=2 |
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|max speed kmh= |
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|prop name=fixed pitch propeller |
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|max speed mph= |
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|prop dia m=<!-- propeller aircraft --> |
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|prop dia ft=<!-- propeller aircraft --> |
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|prop dia in=<!-- propeller aircraft --> |
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|prop dia note= |
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|stall speed kmh=<!-- aerobatic and STOL aircraft --> |
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|stall speed mph=<!-- aerobatic and STOL aircraft --> |
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Performance |
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|range km= |
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|range miles= |
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|max speed kmh=175 |
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|endurance h=<!-- if range unknown --> |
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|max speed note=to {{cvt|180|km/h|mph+kn}} |
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|endurance min=<!-- if range unknown --> |
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|cruise speed kmh= |
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|ceiling m= |
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|cruise speed mph= |
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|ceiling ft= |
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|cruise speed kts= |
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|g limits=<!-- aerobatic aircraft --> |
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|cruise speed note= |
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|roll rate=<!-- aerobatic aircraft --> |
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|stall speed kmh=65 |
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|never exceed speed kmh= |
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|never exceed speed mph= |
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|never exceed speed kts= |
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|never exceed speed note= |
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|range km=1000 |
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|combat range km= |
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|combat range miles= |
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|combat range nmi= |
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|combat range note= |
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|ferry range km= |
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|ferry range miles= |
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|ferry range nmi= |
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|ferry range note= |
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|endurance=6.5 hours |
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|ceiling m=4000 |
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|g limits=<!-- aerobatic --> |
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|roll rate=<!-- aerobatic --> |
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|glide ratio=<!-- sailplanes --> |
|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
|climb rate ms= |
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|climb rate ftmin= |
|climb rate ftmin= |
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|climb rate note= |
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|time to altitude= |
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|sink rate ftmin=<!-- sailplanes --> |
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|wing loading kg/m2=42.5 |
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|fuel consumption kg/km= |
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|armament1= |
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|fuel consumption lb/mi= |
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|armament2= |
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|power/mass={{cvt|0.05682|hp/lb|kW/kg|order=flip}} |
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|armament3= |
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|more performance= |
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|armament4= |
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|armament5= |
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|armament6= |
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}} |
}} |
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==References== |
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<!-- ==See also== --> |
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{{commons category|IMAM Ro.5}} |
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{{aircontent |
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|see also= |
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|related=<!-- related developments --> |
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|similar aircraft=<!-- similar or comparable aircraft --> |
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|lists=<!-- related lists --> |
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}} |
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==Notes== |
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{{reflist}} |
{{reflist}} |
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{{IMAM aircraft}} |
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==References== |
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{{Portal bar|Italy|Companies|Aviation}} |
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* {{cite book |title=The Illustrated Encyclopedia of Aircraft |publisher=Aerospace Publishing|location=London |pages= }} |
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* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages= }} |
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* {{cite book |title=World Aircraft Information Files |publisher=Bright Star Publishing|location=London |pages= }} |
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<!-- ==External links== --> |
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{{Aviation lists}} |
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[[Category: ]] |
[[Category:IMAM aircraft|Ro.05]] |
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[[Category:1920s Italian sport aircraft]] |
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[[Category:Parasol-wing aircraft]] |
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[[Category:Single-engined tractor aircraft]] |
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[[Category:Aircraft first flown in 1929]] |
Latest revision as of 16:15, 30 January 2023
Ro.5 | |
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Role | Sport aircraft |
National origin | Italy |
Manufacturer | IMAM |
Designer | Alessandro Tonini |
First flight | 1929 |
The IMAM Ro.5 was a sport aircraft designed by Alessandro Tonini and produced by IMAM in Italy in the late 1920s.[1]
Design and development
[edit]The Ro.5 was a conventional, parasol wing monoplane with fixed tailskid undercarriage and two open cockpits in tandem.[2] It proved popular with private owners and flying clubs, and was built in large numbers.[2] Some Ro.5s were purchased by the Regia Aeronautica for use as trainers and liaison aircraft.[2] A later version, the Ro.5bis, enclosed the cockpits under a long canopy.[2]
Operators
[edit]Specifications (Ro.5)
[edit]Data from Jane's all the World's Aircraft 1928,[3] The Illustrated Encyclopedia of Aircraft[2]
General characteristics
- Crew: 2
- Length: 6.94 m (22 ft 9 in)
- Wingspan: 10 m (32 ft 10 in)
- Height: 2.16 m (7 ft 1 in)
- Wing area: 16 m2 (170 sq ft)
- Empty weight: 400 kg (882 lb)
- Gross weight: 680 kg (1,499 lb)
- Powerplant: 1 × Walter NZ 85 7-cyl. air-cooled radial piston engine, 63 kW (85 hp)
- Propellers: 2-bladed fixed pitch propeller
Performance
- Maximum speed: 175 km/h (109 mph, 94 kn) to 180 km/h (110 mph; 97 kn)
- Stall speed: 65 km/h (40 mph, 35 kn)
- Range: 1,000 km (620 mi, 540 nmi)
- Endurance: 6.5 hours
- Service ceiling: 4,000 m (13,000 ft)
- Wing loading: 42.5 kg/m2 (8.7 lb/sq ft)
- Power/mass: 0.09341 kW/kg (0.05682 hp/lb)
References
[edit]Wikimedia Commons has media related to IMAM Ro.5.
- ^ Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 768.
- ^ a b c d e The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing. p. 2193.
- ^ Grey, C.G., ed. (1928). Jane's all the World's Aircraft 1928. London: Sampson Low, Marston & company, ltd. p. 169c.