Engineering:Astra C

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Short description: French single engine aircraft
Astra C
Astra CM sk.jpg
Astra CM Hydro-avion
Role Sports plane and observation aircraft
Manufacturer Société Astra
First flight 1912

The Astra C was a 1912 French single engine biplane, manufactured by Société Astra at Villacoublay. In 1913, the Astra CM Hydro-avion three-seat floatplane version was used to make the world's first scheduled passenger-carrying flights.

Design and development

The Astra C was initially designed as a single seat biplane, powered by a single 50 hp Renault engine in tractor configuration. It was constructed primarily as wooden framework sections, covered in canvas and wire-braced. The fuselage was of triangular cross section, with a wheeled main undercarriage plus nose skid and tail skid. The wings were of unequal span, and employed wing-warping for roll control.[1]

The Astra CM was developed from the Astra C, with a more powerful engine and added accommodation for two observers, for military reconnaissance.[1][2][3]

The Astra Hydro, (an Astra CM 'Hydro-avion' (seaplane)), was a further development in 1913, with a 75 kW (100 hp) Renault V-12 engine and 3 Tellier floats (2 main floats 4.5 m × 1.15 m (14.8 ft × 3.8 ft), and one small tail float). The wooden frame elements were largely replaced by steel tubes, and the wing ribs and floats were the principal remaining wooden components.[4] at least two were built and an order for two from the Royal Navy (RN), serialled 106 and 107, was not completed.[5]

Operational history

During the St. Malo races, 14-26 August 1912, the first CM Hydro was flown to first place by Labouret. The second CM Hydro, powered by a horizontally mounted 82 kW (110 hp) Salmson M.9 water-cooled radial engine, flew at Monaco but crashed.

On 22 March 1913, using at least one Astra CM Hydro-avion, French operator Compagnie générale transaérienne started the world's first scheduled passenger-carrying flights, operating from Cannes to Nice. Two passengers could be carried. On 29 March 1913, the service was extended to Monte Carlo.[6][7]

Variants

Astra C
Civil version, with 50 hp Renault engine.[8]
Astra CM
Military version, with 75 hp Renault or 75 hp Chenu engine.[8]
Astra Hydro
Floatplane version of the Astra CM, with 100 hp Renault engine.[8]

Operators

 France
  • Compagnie générale transaérienne
 Greece
  • Royal Hellenic Navy
    • Hellenic Naval Air Service

Specifications (Astra CM)

General characteristics

  • Crew: one pilot
  • Capacity: two observers
  • Length: 10.97 m (36 ft 0 in)
  • Wingspan: 12.32 m (40 ft 5 in)
  • Wing area: 48.2 m2 (519 sq ft)
  • Empty weight: 673 kg (1,484 lb)
  • Gross weight: 1,000 kg (2,200 lb)
  • Powerplant: 1 × Renault , 63 kW (85 hp)

Performance

  • Maximum speed: 85 km/h (53 mph, 46 kn)

References

  1. 1.0 1.1 Parmentier, Bruno (27 May 1998). "Astra CM" (in fr). http://www.aviafrance.com/astra-cm-aviation-france-4490.htm. 
  2. "Paris Air Show". Flight 3 No. 52 (157): 1130–1137. 30 December 1911. https://www.flightglobal.com/pdfarchive/view/1911/1911%20-%201122.html. Retrieved 8 September 2018. 
  3. Naughton, Russell. The Pioneers : An Anthology : Astra, Astra-Wright. https://www.ctie.monash.edu.au/hargrave/astra.html. Retrieved 8 September 2018. 
  4. Flight, 16 November 1912, p. 1053
  5. Opdycke, Leonard E. (1999). French Aeroplanes before the Great War. Atglen: Schiffer Publishing Limited. pp. 28-30. ISBN 0-7643-0752-5. https://archive.org/details/frenchaeroplanes00opdy. 
  6. Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. 
  7. Jung, Philippe. 2010. Alpes-Maritimes & Monaco Aerospace History
  8. 8.0 8.1 8.2 Jane, Fred T. (1969). Jane's all the world's aircraft, 1913. New York: Arco Publishing Co. p. 79. https://catalog.hathitrust.org/Record/009905437. 

Bibliography

  • Thomas, Andrew. "In the Footsteps of Daedulus: Early Greek Naval Aviation". Air Enthusiast, No. 94, July–August 2001, pp. 8–9. ISSN 0143-5450

Further reading

External links