R.XI
Role Heavy fighter
Manufacturer Caudron
Designer Paul Deville[1]
First flight 1916[2]
Introduction 1918[2]
Retired July 1922
Primary user France
Produced 1917-1918
Number built 370
Developed from Caudron R.4
Caudron R.XI posed for official type photos, showing large balanced rudder and fin.

The Caudron R.11 (or R.XI in contemporary usage), was a French three-seat twin-engine long range escort fighter biplane developed and produced by Caudron during the First World War.[2]

Development

The R.XI was intended to fulfill a French Corps d'Armee requirement for a long range three-seat escort fighter. Its design was similar to the Caudron R.4, but without a nose-wheel, and with longer wings and fuselage, with two bracing bays outboard the engines rather than three, along with a much larger tail. Hispano-Suiza 8Ba liquid-cooled V-8 engines were housed in streamlined nacelles just above the lower wing, fitted with frontal radiators, which replaced the air-cooled Renault engines used in the R.4.

Operational history

Production of the 1000 R.XIs ordered by the French Army began in 1917, with the first aircraft completed late in that year.[1]

The first escadrille, R 46, was equipped with the type in February 1918 and the last escadrille to form was R 246,[3] before the Armistice resulted in an abrupt end to production, at which point approximately 370 aircraft had been completed by Caudron, Régy Frères and Gremont.[1]

Variants

Caudron R.XI C.3
Heavy escort fighter with 160 kW (215 hp) Hispano-Suiza 8Bda engines.
Caudron R.XII C.3
R.XI with the more powerful 220 kW (300 hp) Hispano-Suiza 8Fb engines that were expected to boost performance. Sources differ, but it may have had a slightly increased wing area, to 60 m2 (650 sq ft) and an extra wing bay was added outboard of the engines. It first flew in November 1918 but was still undergoing testing in mid-1919 and no production followed despite plans to equip 12 escadrilles.[4]
Caudron R.XIV Ca.3
Similar to the R.XII, but armed with a 37 mm (1.5 in) Hotchkiss cannon in addition to the normal complement of 5 machine guns, and with further increased wing area, to 63 m2 (680 sq ft), and a larger, unbalanced rudder. A single example was built following the conversion of an R.XI to carry the cannon in August 1918.[4]

Operators

R.XI nose and engine nacelle detail
 France
 United Kingdom
 United States

Specifications (Caudron R.XI C.3)

Caudron R.11 drawing

Data from Davilla, 1997, p.168

General characteristics

  • Crew: 3
  • Length: 11.22 m (36 ft 10 in)
  • Upper wingspan: 17.92 m (58 ft 10 in)
  • Lower wingspan: 16.97 m (55 ft 8 in)
  • Height: 2.8 m (9 ft 2 in)
  • Wing area: 54.25 m2 (583.9 sq ft)
  • Empty weight: 1,422 kg (3,135 lb)
  • Gross weight: 2,165 kg (4,773 lb)
  • Fuel capacity: 220 L (48 imp gal; 58 US gal)[5][6]
  • Powerplant: 2 × Hispano-Suiza 8Bda V-8 water-cooled piston engines, 160 kW (215 hp) each
  • Propellers: 2-bladed wooden fixed pitch propellers

Performance

  • Maximum speed: 190 km/h (120 mph, 100 kn) at sea level[5]
  • 183 km/h (114 mph) at 2,000 m (6,600 ft)
  • 178 km/h (111 mph) at 3,000 m (9,800 ft)
  • 173 km/h (107 mph) at 4,000 m (13,000 ft)
  • 164 km/h (102 mph) at 5,000 m (16,000 ft)
  • Range: 600 km (370 mi, 320 nmi)
  • Endurance: 3 hours
  • Service ceiling: 5,950 m (19,520 ft)
  • Time to altitude:
  • 2,000 m (6,600 ft) in 8 minutes 10 seconds
  • 3,000 m (9,800 ft) in 14 minutes 30 seconds
  • 4,000 m (13,000 ft) in 22 minutes 30 seconds
  • 5,000 m (16,000 ft) in 39 minutes
  • Wing loading: 39.9 kg/m2 (8.18 lb/sq ft) [7]
  • Power/mass: 18.08 kW/kg (11.00 hp/lb)[7]

Armament

Related development

Aircraft of comparable role, configuration, and era

  • SPAD SA.3
  • Ponnier P.1

References

Wikimedia Commons has media related to Caudron R.11.

Notes

  1. 1 2 3 Davilla, 1997, p.167
  2. 1 2 3 Davilla, 1997, p.168
  3. 1 2 3 4 5 6 7 8 9 Davilla, 1997, p.169
  4. 1 2 Davilla, 1997, p.170
  5. 1 2 Green and Swanborough 1994, p.111.
  6. ↑ Grey, C.G. (1969). Jane's all the World's Aircraft 1919 (Facsimile ed.). London: David & Charles (Publishers) Limited. p. 224a. ISBN 0715346474.
  7. 1 2 French aeroplanes in service at the front, 1919, p.204

Bibliography

  • Cony, Christophe (August 1997). "Aviateur d'Observation en 14/18 (3ème partie et fin)" [Aircraft observers in 1914-1918 (third and final part)]. Avions: Toute l'aéronautique et son histoire (in French). No. 53. pp. 16–21. ISSN 1243-8650.
  • Davilla, J. J.; Soltan, A. (1997). French Aircraft of the First World War. Mountain View, CA: Flying Machines Press. ISBN 978-1891268090.
  • "French aeroplanes in service at the front". Flight. 13 February 1919. p. 204.
  • Green, W.; Swanborough, G (1994). The Complete Book of Fighters. New York: Smithmark. ISBN 0-8317-3939-8.
  • Owers, Colin A. (2013). Caudron R.11. Windsock Datafile No. 161. Albatros Productions. ISBN 978-1906798338.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.