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<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
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{|{{Infobox |
{|{{Infobox aircraft begin |
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| name=C.530 Rafale |
| name=C.530 Rafale |
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| image= |
| image=Caudron C530..png |
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| caption= |
| caption= |
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}}{{Infobox |
}}{{Infobox aircraft type |
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| type=Two seat [[racing aircraft|racing]] and [[sports aircraft]] |
| type=Two seat [[racing aircraft|racing]] and [[sports aircraft]] |
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| national origin=[[France]] |
| national origin=[[France]] |
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| manufacturer=[[Caudron|Société des Avions Caudron]] |
| manufacturer=[[Caudron|Société des Avions Caudron]] |
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| designer=Marcel Riffard |
| designer=[[Marcel Riffard]] |
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| first flight= |
| first flight=early 1934 |
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| introduced= |
| introduced= |
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| retired= |
| retired= |
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The '''Caudron C.530 Rafale''' ({{lang-en|Gust}}) was a [[france|French]] two seat competition aircraft. Only seven were built but they had great success in several contests during 1934. |
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The '''Caudron C.530 Rafale''' was a |
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==Design and development== |
==Design and development== |
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The C.530 was a [[low wing]] [[cantilever]] [[monoplane]], wood framed and [[aircraft fabric covering|fabric covered]]. Its wing was tapered, round tipped and carried [[flap (aircraft)|split flaps]]. Its [[fuselage]] was flat sided, with a deep, rounded decking running the full length. It had |
The C.530 was a [[low wing]] [[cantilever]] [[monoplane]], wood framed and [[aircraft fabric covering|fabric covered]], with a good deal in common with its predecessor and namesake, the [[Caudron C.430 Rafale]], though with a lower [[wing loading]]. Its wing was tapered, round tipped and carried [[flap (aircraft)|split flaps]]. Its [[fuselage]] was flat sided, with a deep, rounded decking running the full length. It had an [[air-cooled engine|air cooled]] {{convert|152|hp|kW|abbr=on|0|order=flip}} Renault Bengali Junior inverted four cylinder [[straight engine|inline engine]] in the nose, driving a two blade, variable [[blade pitch|pitch]] [[propeller (aircraft)|propeller]]. This engine was a version of the [[Renault 4P]] with its compression increased to 6:1 and running at the higher speed of 2,450 rpm. The Rafale's two seats were in tandem, one over the wing and the other just behind the [[trailing edge]], under a long (about a third of the fuselage length), narrow [[aircraft canopy|multi-framed canopy]] with a blunt, vertical windscreen and sliding access. Behind the canopy a long [[aircraft fairing|fairing]] continued its profile to the straight tapered, round tipped vertical tail. The horizontal tail was mounted largely ahead of the [[fin]] on the top of the fuselage.<ref name=Flight34B/> |
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The Rafale had a fixed [[landing gear| |
The Rafale had a fixed [[landing gear|wide track, tailskid undercarriage]]. Its wheels were on vertical, slender [[aerofoil]] section legs from the wings and were largely enclosed within magnesium alloy fairings.<ref name=Flight34B/> |
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The |
The date of the first flight is not certain but it was certainly flying by 7 June 1934,<ref name=Flight34C/> possibly for the first time.<ref name=afr/> Another six examples built were registered soon after.<ref name=FrReg/> |
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==Operational history== |
==Operational history== |
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The C.530 Rafale was intended as competition aircraft and in 1934 it was very successful. On 8 July Rafales took the first three places in the Angers 12 hour event<ref name=Flight34A/> |
The C.530 Rafale was intended asa competition aircraft and in 1934 it was very successful. On 8 July Rafales took the first three places in the Angers 12 hour event<ref name=Flight34A/> and later that month filled the top six Esders Cup positions.<ref name=Flight34B/><ref name=Laero34A/> Late in August, one won the Zénith Cup with a flight over the prescribed {{convert|1578|km|mi|abbr=on|0}} course at {{convert|240|km/h|mph|abbr=on|1|}}.<ref name=Laero34B/> |
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Coupe Esders<ref name=Flight34B/><ref name=Laero34A/> Coupe Zénith<ref name=Laero34B/> |
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In 1935 two of the C.530s were converted into '''C.660 Rafale'''s, powered by Renault {{convert|180|hp|kW|abbr=on|0|order=flip}} six cylinder inverted inline engines. One of these won that year's Angers 12 hour event.<ref name=FrReg/><ref name=Flight35/> |
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==Specifications== |
==Specifications== |
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|crew=Two |
|crew=Two |
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|capacity= |
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|length m=7.50 |
|length m=7.50 |
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|length note=<ref name=afr/> |
|length note=<ref name=afr/> |
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|eng1 number=1 |
|eng1 number=1 |
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|eng1 name=[[Renault 4P|Renault Bengali Sport]] |
|eng1 name=[[Renault 4P|Renault Bengali Sport]] |
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|eng1 type=4 cylinder, air cooled, inverted [[straight engine|inline]] |
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|eng1 type= |
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|eng1 kw=<!-- prop engines --> |
|eng1 kw=<!-- prop engines --> |
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|eng1 hp=152 |
|eng1 hp=152 |
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|prop blade number=2 |
|prop blade number=2 |
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|prop name= |
|prop name=[[Ratier]], automatic variable [[blade pitch|pitch]], adjustable in flight<ref name=Flight34B/> |
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|prop dia m=<!-- propeller aircraft --> |
|prop dia m=<!-- propeller aircraft --> |
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|prop dia ft=<!-- propeller aircraft --> |
|prop dia ft=<!-- propeller aircraft --> |
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|fuel consumption kg/km= |
|fuel consumption kg/km= |
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|fuel consumption lb/mi= |
|fuel consumption lb/mi= |
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|power/mass |
|power/mass= |
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|more performance= |
|more performance= |
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*'''Take-off:''' in {{convert|160|m|ft|abbr=on |
*'''Take-off:''' in {{convert|160|m|ft|0|abbr=on}}, at less than {{convert|90|km/h|mph|0|abbr=on}} |
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}} |
}} |
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==References== |
==References== |
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{{columns-list|colwidth=30em| |
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{{reflist|refs= |
{{reflist|refs= |
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<ref name=Flight34A>{{cite |
<ref name=Flight34A>{{cite magazine |date= 19 July 1934 |title=Les Douze Heures d'Angers|magazine= [[Flight International|Flight]]|volume=XXVI|issue=1334 |page=743 |url= http://www.flightglobal.com/pdfarchive/view/1934/1934%20-%200741.html }}</ref> |
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<ref name=Flight34B>{{cite |
<ref name=Flight34B>{{cite magazine|date=9 August 1934 |title= Racing at Deauville|magazine=[[Flight International|Flight]]|volume=XXVI|issue=1337|page=857|url= http://www.flightglobal.com/pdfarchive/view/1934/1934%20-%200805.html }}</ref> |
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<ref name= |
<ref name=Flight34C>{{cite magazine|date=7 June 1934 |title= Vincennes again|magazine=[[Flight International|Flight]]|volume=XXVI|issue=1328|page=807|url= http://www.flightglobal.com/pdfarchive/view/1934/1934%20-%200567.html }}</ref> |
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<ref name=Flight35>{{cite magazine|date=18 July 1935 |title= The Douze Heures d'Angers|magazine=[[Flight International|Flight]]|volume=XXVIII|issue=1386|page=83|url= http://www.flightglobal.com/pdfarchive/view/1935/1935%20-2-%200099.html }}</ref> |
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<ref name= |
<ref name=Laero34A>{{cite magazine |date=26 July 1934 |title=L'Aviation Sportive|magazine=L'Aérophile|volume=14 |issue=684 |page=8|url=http://gallica.bnf.fr/ark:/12148/bpt6k6576049f/f8.image}}</ref> |
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http://gallica.bnf.fr/ark:/12148/bpt6k6553682n/f21.image}}</ref> |
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<ref name= |
<ref name=Laero34B>{{cite magazine |date=July 1935 |title=Le Coupe Zénith|magazine=L'Aérophile|volume=42|issue=9|page=267|url=http://gallica.bnf.fr/ark:/12148/bpt6k6553682n/f21.image}}</ref> |
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<ref name=GC>{{cite journal |date=8 December 1934 |title=La XIV Exposition Internationale de l'Aéronautique, Paris 1934|journal=Le Génie Civil |volume=CV|issue=23|pages=524–5|url=http://gallica.bnf.fr/ark:/12148/bpt6k64853837/f5.image}}</ref> |
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<ref name=FrReg>http://www.ab-ix.co.uk/f-aaaa.pdf</ref> |
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<ref name= |
<ref name=FrReg>{{Cite web |url=http://www.ab-ix.co.uk/f-aaaa.pdf |title=Archived copy |access-date=2015-03-06 |archive-date=2012-07-25 |archive-url=https://web.archive.org/web/20120725223830/http://www.ab-ix.co.uk/f-aaaa.pdf |url-status=dead }}</ref> |
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<ref name=afr>{{cite web |url=http://www.aviafrance.com/caudron-c-530-rafale--aviation-france-9841.htm|title=Caudron C.530 |accessdate=2 March 2015}}</ref> |
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}} |
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}} |
}} |
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{{Caudron aircraft}} |
{{Caudron aircraft}} |
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{{Aviation lists}} |
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[[ |
[[Category:Caudron aircraft|C.530]] |
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[[Category:1930s French sport aircraft]] |
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[[Category:Single-engined tractor aircraft]] |
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[[Category:Low-wing aircraft]] |
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[[Category:Aircraft first flown in 1934]] |
C.530 Rafale | |
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![]() | |
Role | Two seat racing and sports aircraft
Type of aircraft
|
National origin | France |
Manufacturer | Société des Avions Caudron |
Designer | Marcel Riffard |
First flight | early 1934 |
Number built | 7 |
The Caudron C.530 Rafale (English: Gust) was a French two seat competition aircraft. Only seven were built but they had great success in several contests during 1934.
The C.530 was a low wing cantilever monoplane, wood framed and fabric covered, with a good deal in common with its predecessor and namesake, the Caudron C.430 Rafale, though with a lower wing loading. Its wing was tapered, round tipped and carried split flaps. Its fuselage was flat sided, with a deep, rounded decking running the full length. It had an air cooled 113 kW (152 hp) Renault Bengali Junior inverted four cylinder inline engine in the nose, driving a two blade, variable pitch propeller. This engine was a version of the Renault 4P with its compression increased to 6:1 and running at the higher speed of 2,450 rpm. The Rafale's two seats were in tandem, one over the wing and the other just behind the trailing edge, under a long (about a third of the fuselage length), narrow multi-framed canopy with a blunt, vertical windscreen and sliding access. Behind the canopy a long fairing continued its profile to the straight tapered, round tipped vertical tail. The horizontal tail was mounted largely ahead of the fin on the top of the fuselage.[1]
The Rafale had a fixed wide track, tailskid undercarriage. Its wheels were on vertical, slender aerofoil section legs from the wings and were largely enclosed within magnesium alloy fairings.[1]
The date of the first flight is not certain but it was certainly flying by 7 June 1934,[2] possibly for the first time.[3] Another six examples built were registered soon after.[4]
The C.530 Rafale was intended as a competition aircraft and in 1934 it was very successful. On 8 July Rafales took the first three places in the Angers 12 hour event[5] and later that month filled the top six Esders Cup positions.[1][6] Late in August, one won the Zénith Cup with a flight over the prescribed 1,578 km (981 mi) course at 240 km/h (149.1 mph).[7]
In 1935 two of the C.530s were converted into C.660 Rafales, powered by Renault 134 kW (180 hp) six cylinder inverted inline engines. One of these won that year's Angers 12 hour event.[4][8]
Data from Le Génie Civil December 1934[9]
General characteristics
Performance
{{cite web}}
: CS1 maint: archived copy as title (link)
Caudron aircraft
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Letter designators & Early |
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Gaston Caudron (G) types |
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René Caudron (R) types |
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Numerical Designations |
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Messerschmitt-Caudron |
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Names |
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