Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 Design and development  





2 Operational history  





3 Specifications  





4 References  














Caudron C.530 Rafale






Ελληνικά
فارسی
Français
Тоҷикӣ
 

Edit links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 




Print/export  



















Appearance
   

 






From Wikipedia, the free encyclopedia
 


This is an old revision of this page, as edited by TSRL (talk | contribs)at20:26, 27 February 2022 (Operational history: typo). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.
(diff)  Previous revision | Latest revision (diff) | Newer revision  (diff)

C.530 Rafale
Role Two seat racing and sports 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.

Design and development

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]

Operational history

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]

Specifications

Data from Le Génie Civil December 1934[9]

General characteristics

Performance

References

  1. ^ a b c d "Racing at Deauville". Flight. Vol. XXVI, no. 1337. 9 August 1934. p. 857.
  • ^ "Vincennes again". Flight. Vol. XXVI, no. 1328. 7 June 1934. p. 807.
  • ^ a b c "Caudron C.530". Retrieved 2 March 2015.
  • ^ a b http://www.ab-ix.co.uk/f-aaaa.pdf [dead link]
  • ^ "Les Douze Heures d'Angers". Flight. Vol. XXVI, no. 1334. 19 July 1934. p. 743.
  • ^ "L'Aviation Sportive". L'Aérophile. Vol. 14, no. 684. 26 July 1934. p. 8.
  • ^ "Le Coupe Zénith". L'Aérophile. Vol. 42, no. 9. July 1935. p. 267.
  • ^ "The Douze Heures d'Angers". Flight. Vol. XXVIII, no. 1386. 18 July 1935. p. 83.
  • ^ "La XIV Exposition Internationale de l'Aéronautique, Paris 1934". Le Génie Civil. CV (23): 524–5. 8 December 1934.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Caudron_C.530_Rafale&oldid=1074352143"

    Categories: 
    Caudron aircraft
    1930s French sport aircraft
    Single-engined tractor aircraft
    Low-wing aircraft
    Aircraft first flown in 1934
    Hidden categories: 
    All articles with dead external links
    Articles with dead external links from February 2022
    Articles with short description
    Short description matches Wikidata
    Articles containing explicitly cited English-language text
    Aircraft specs templates using more performance parameter
     



    This page was last edited on 27 February 2022, at 20:26 (UTC).

    This version of the page has been revised. Besides normal editing, the reason for revision may have been that this version contains factual inaccuracies, vandalism, or material not compatible with the Creative Commons Attribution-ShareAlike License.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Mobile view



    Wikimedia Foundation
    Powered by MediaWiki