Macchi M.19: Difference between revisions
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{{Infobox |
{|{{Infobox aircraft begin |
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|name=Macchi M.19 |
|name=Macchi M.19 |
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|image= |
|image=Macchi M.19.jpg |
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|caption= |
|caption= |
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}}{{Infobox aircraft type |
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|type=Racing flying boat |
|type=Racing flying boat |
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|manufacturer=[[Macchi]] |
|manufacturer=[[Aermacchi|Macchi]] |
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|designer= |
|designer= |
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|first flight= |
|first flight=1920 |
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|introduced= |
|introduced= |
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|retired= |
|retired=1921 |
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|status= |
|status= |
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|primary user= |
|primary user= |
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|variants with their own articles= |
|variants with their own articles= |
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==Development== |
==Development== |
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Based on the earlier [[Macchi M.17]] racer the M.19 first flew in August |
Based on the earlier [[Macchi M.17]] racer the M.19 first flew in August 1920. It was designed to meet a new [[Schneider Trophy]] rule that each competitor should carry 300 kg (660 lb) of disposable load. It was a single-seat [[biplane]] flying boat with a 490 kW (650 hp) [[Fiat A.14]] engine strut-mounted above the upper wing, driving a four-blade propeller in [[tractor configuration]]. |
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Early test flights showed a torque reaction from the powerful engine and the hull and [[rudder]] had to be redesigned. This resulted in the M.19 missing the 1920 Schneider race. The following year the weight rule was relaxed. In the 1921 race, the M.19 competed against two [[Macchi M.7|M.7]]s, but the M.19 had to be withdrawn after the 12th lap with a fractured crankshaft which ruptured a fuel line, causing the aircraft to catch fire. |
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{{aerospecs |
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|ref= |
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|met or eng?=<!-- eng for US/UK aircraft, met for all others -->met |
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{{Aircraft specs |
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|capacity= |
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|prime units? = met |
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|length m= |
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|length ft= |
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|length in= |
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|span m=15.86 |
|span m=15.86 |
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|span ft=52 |
|span ft=52 |
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|span in=0 |
|span in=0.5 |
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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 --> |
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|empty weight kg= |
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|empty weight lb= |
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|gross weight kg= |
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|gross weight lb= |
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|lift kg=<!-- lighter-than-air --> |
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|lift lb=<!-- lighter-than-air --> |
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|eng1 number=1 |
|eng1 number=1 |
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|eng1 |
|eng1 name=[[Fiat A.14]] V12 in-line engine |
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|eng1 kw= |
|eng1 kw=490 |
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|eng1 hp= |
|eng1 hp=650 |
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|eng1 kn=<!-- jet/rocket engines --> |
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|eng1 lbf=<!-- jet/rocket engines --> |
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|eng1 kn-ab=<!-- afterburners --> |
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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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|max speed kmh=240 |
|max speed kmh=240 |
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|max speed mph=149 |
|max speed mph=149 |
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|max speed mach=<!-- supersonic aircraft --> |
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|cruise speed kmh=<!-- if max speed unknown --> |
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|cruise speed mph=<!-- if max speed unknown --> |
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|range km= |
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|range miles= |
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|endurance h=<!-- if range unknown --> |
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|endurance min=<!-- if range unknown --> |
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|ceiling m= |
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|ceiling ft= |
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|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
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|climb rate ftmin= |
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|sink rate ms=<!-- sailplanes --> |
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|sink rate ftmin=<!-- sailplanes --> |
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|armament1= |
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|armament2= |
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|armament3= |
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|armament4= |
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|armament5= |
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|armament6= |
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}} |
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|related=<!-- related developments --> |
|related=<!-- related developments --> |
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|similar aircraft=<!-- similar or comparable aircraft --> |
|similar aircraft=<!-- similar or comparable aircraft --> |
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|sequence=<!-- designation sequence, if appropriate --> |
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|lists=<!-- related lists --> |
|lists=<!-- related lists --> |
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*[[List of |
*[[List of flying boats and floatplanes]] |
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}} |
}} |
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==References== |
==References== |
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{{commons category|Macchi M.19}} |
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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 |last= |first= |
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London }} |
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*{{cite book |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985)|publisher= Orbis Publishing|pages=2395}} |
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<!-- ==External links== --> |
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{{Macchi aircraft}} |
{{Macchi aircraft}} |
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{{Portal bar|Italy|Companies|Aviation}} |
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{{aviation lists}} |
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[[Category: |
[[Category:Macchi aircraft|M.19]] |
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[[Category: |
[[Category:1920s Italian experimental aircraft]] |
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[[Category: |
[[Category:Flying boats]] |
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[[Category:Biplanes]] |
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[[Category:Single-engined tractor aircraft]] |
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[[Category:Aircraft first flown in 1920]] |
Latest revision as of 17:00, 13 August 2024
Macchi M.19 | |
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Role | Racing flying boat |
Manufacturer | Macchi |
First flight | 1920 |
Retired | 1921 |
Number built | 1 |
The Macchi M.19 was a 1920s Italian single-seat racing flying boat designed and built by Macchi for the 1920 Schneider Trophy race.
Development
[edit]Based on the earlier Macchi M.17 racer the M.19 first flew in August 1920. It was designed to meet a new Schneider Trophy rule that each competitor should carry 300 kg (660 lb) of disposable load. It was a single-seat biplane flying boat with a 490 kW (650 hp) Fiat A.14 engine strut-mounted above the upper wing, driving a four-blade propeller in tractor configuration.
Early test flights showed a torque reaction from the powerful engine and the hull and rudder had to be redesigned. This resulted in the M.19 missing the 1920 Schneider race. The following year the weight rule was relaxed. In the 1921 race, the M.19 competed against two M.7s, but the M.19 had to be withdrawn after the 12th lap with a fractured crankshaft which ruptured a fuel line, causing the aircraft to catch fire.
Specifications (M.19)
[edit]General characteristics
- Crew: one
- Wingspan: 15.86 m (52 ft 0.5 in)
- Powerplant: 1 × Fiat A.14 V12 in-line engine , 490 kW (650 hp)
Performance
- Maximum speed: 240 km/h (149 mph, 129 kn)
See also
[edit]Related lists
References
[edit]- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing. p. 2395.