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CAMS 30E

The CAMS 30E was a two-seat flying boat trainer built in France in the early 1920s. It was the first aircraft designed for CAMS by Raffaele Conflenti after he had been recruited by the company from his previous job at Società Idrovolanti Alta Italia (SIAI). It was a conventional design for the era featuring a two-bay equal-span unstaggered biplane wing cellule. The prototype was exhibited at the 1922 Salon de l'Aéronautique and evaluated the following year by the Aéronautique Maritime. The type's favourable performance led to an order of 22 machines for the French military and an export order of seven for Yugoslavia and four for Poland.

CAMS 30
A CAMS 30E
Role Flying boat trainer
Manufacturer CAMS
Designer Raffaele Conflenti
First flight 1922
Number built 31
Variants CAMS 46ET

A single civil example was produced as the CAMS 30T with two extra passenger seats. In August 1924, Ernest Burri used this machine to break the world air speed record for a passenger-carrying seaplane.

Variants

  • CAMS 30E - Production military flying-boat trainer.[1]
  • CAMS 30T - Passenger version of the CAMS30E with two extra seats.
 
A CAMS 30T

Operators

  France
  Kingdom of Yugoslavia
  Poland

Specifications (30E)

Data from Jane's all the World's Aircraft 1924,[2] Aviafrance:CAMS 30E[1]

General characteristics

  • Crew: 2
  • Length: 9.28 m (30 ft 5 in)
  • Wingspan: 12.4 m (40 ft 8 in)
  • Height: 3.12 m (10 ft 3 in)
  • Wing area: 43 m2 (460 sq ft)
  • Empty weight: 885 kg (1,951 lb)
  • Gross weight: 1,180 kg (2,601 lb)
  • Powerplant: 1 × Hispano-Suiza 8Aa V-8 water-cooled piston engine, 110 kW (150 hp)

Performance

  • Maximum speed: 153 km/h (95 mph, 83 kn)
  • Wing loading: 27.5 kg/m2 (5.6 lb/sq ft)
  • Power/mass: 0.0893 kW/kg (0.0543 hp/lb)

References

  1. ^ a b Parmentier, Bruno. "C.A.M.S. 30E". Aviafrance (in French). Paris. Retrieved 11 March 2018.
  2. ^ Grey, C.G., ed. (1924). Jane's all the World's Aircraft 1924. London: Sampson Low, Marston & company, ltd. p. 107b.

Bibliography

  • Cortet, Pierre (November 1999). "Les hydroavions CAMS 30E" [The CAMS 30E Seaplane]. Avions: Toute l'Aéronautique et son histoire (in French) (80): 20–23. ISSN 1243-8650.
  • Isaic, Vladimir (May 1999). "Les hydroavions CAMS 30e en Yugoslavie" [Yugoslav CAMS 30e Seaplanes]. Avions: Toute l'Aéronautique et son histoire (in French) (74): 42–49. ISSN 1243-8650.
  • Nelcarz, Bartolomiej & Peczkowski, Robert (April 2000). "Les appareils français dans la Marine Polonaise" [French Aircraft of the Polish Navy]. Avions: Toute l'Aéronautique et son histoire (in French) (85): 22–27. ISSN 1243-8650.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 225.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 891 Sheet 01.

cams, seat, flying, boat, trainer, built, france, early, 1920s, first, aircraft, designed, cams, raffaele, conflenti, after, been, recruited, company, from, previous, società, idrovolanti, alta, italia, siai, conventional, design, featuring, equal, span, unsta. The CAMS 30E was a two seat flying boat trainer built in France in the early 1920s It was the first aircraft designed for CAMS by Raffaele Conflenti after he had been recruited by the company from his previous job at Societa Idrovolanti Alta Italia SIAI It was a conventional design for the era featuring a two bay equal span unstaggered biplane wing cellule The prototype was exhibited at the 1922 Salon de l Aeronautique and evaluated the following year by the Aeronautique Maritime The type s favourable performance led to an order of 22 machines for the French military and an export order of seven for Yugoslavia and four for Poland CAMS 30A CAMS 30ERole Flying boat trainerManufacturer CAMSDesigner Raffaele ConflentiFirst flight 1922Number built 31Variants CAMS 46ETA single civil example was produced as the CAMS 30T with two extra passenger seats In August 1924 Ernest Burri used this machine to break the world air speed record for a passenger carrying seaplane Variants EditCAMS 30E Production military flying boat trainer 1 CAMS 30T Passenger version of the CAMS30E with two extra seats A CAMS 30TOperators Edit FranceAeronautique Maritime Kingdom of YugoslaviaYugoslav Royal Navy PolandSpecifications 30E EditData from Jane s all the World s Aircraft 1924 2 Aviafrance CAMS 30E 1 General characteristicsCrew 2 Length 9 28 m 30 ft 5 in Wingspan 12 4 m 40 ft 8 in Height 3 12 m 10 ft 3 in Wing area 43 m2 460 sq ft Empty weight 885 kg 1 951 lb Gross weight 1 180 kg 2 601 lb Powerplant 1 Hispano Suiza 8Aa V 8 water cooled piston engine 110 kW 150 hp Performance Maximum speed 153 km h 95 mph 83 kn Wing loading 27 5 kg m2 5 6 lb sq ft Power mass 0 0893 kW kg 0 0543 hp lb References Edit Wikimedia Commons has media related to CAMS 30 a b Parmentier Bruno C A M S 30E Aviafrance in French Paris Retrieved 11 March 2018 Grey C G ed 1924 Jane s all the World s Aircraft 1924 London Sampson Low Marston amp company ltd p 107b Bibliography EditCortet Pierre November 1999 Les hydroavions CAMS 30E The CAMS 30E Seaplane Avions Toute l Aeronautique et son histoire in French 80 20 23 ISSN 1243 8650 Isaic Vladimir May 1999 Les hydroavions CAMS 30e en Yugoslavie Yugoslav CAMS 30e Seaplanes Avions Toute l Aeronautique et son histoire in French 74 42 49 ISSN 1243 8650 Nelcarz Bartolomiej amp Peczkowski Robert April 2000 Les appareils francais dans la Marine Polonaise French Aircraft of the Polish Navy Avions Toute l Aeronautique et son histoire in French 85 22 27 ISSN 1243 8650 Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 225 World Aircraft Information Files London Bright Star Publishing pp File 891 Sheet 01 Retrieved from https en wikipedia org w index php title CAMS 30E amp oldid 1002907491, wikipedia, wiki, book, books, library,

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