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Phönix C.I

From Wikipedia, the free encyclopedia
Phönix C.I
General information
TypeReconnaissance and General-Purpose Biplane
National originAustria-Hungary
ManufacturerPhönix Flugzeug-Werke[1]
Primary userKuKLFT[1]
Number built140
History
Introduction date1918
Retired1920s

ThePhönix C.I, given serial numbers in thePhönix 121 range, was anAustro-Hungarian First World War reconnaissance and general-purposebiplane built byPhönix andLloyd.[2]

Development

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The Phönix C.I was the first original design developed by the Phönix Flugzeug-Werke It was based on the Hansa-Brandenburg C.II that Phönix was building under licence.[2] A conventional biplane with a rear fuselage/tailplane similar to aircraft designed byErnst Heinkel.[2] The C.I had a fixed tail-skid landing gear and was powered by a 171.51 kW (230 hp)Hiero 6-cylinder inline piston engine, it had two tandem open cockpits for the pilot and observer/gunner.[2] The company built 110 C.Is and then entered service with theKuKLFT in early 1918.[2] After the First World War 30 aircraft were built by the Swedish Army engineering department fitted with 220 hp (164 kW)Benz Bz.IV inline engines.[2]

Designations and serials

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Phönix C.I aircraft built by Phönix were serialled fromPhönix C.I 121.01 toPhönix C.I 121.160 and Phönix C.I aircraft ordered fromLloyd (Ungarische Lloyd Flugzeug und Motorenfabrik AG) were allocated serials fromPhönix C.I(Ll) 49.01 toPhönix C.I(Ll) 49.100. Some 80 aircraft ordered fromUFAG were not assigned serial numbers, probably due to production being interrupted by theArmistice and 225 more were ordered but not built.[1]

Operators

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Austria-Hungary
 Hungary
 Romania
Sweden
Kingdom of Yugoslavia

Specifications (C.1)

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Data from Austro-Hungarian Army Aircraft of World War One[1]Illustrated Encyclopedia of Aircraft[2]

General characteristics

  • Crew: 2
  • Length: 7.52 m (24 ft 8 in)
  • Upper wingspan: 11 m (36 ft 1 in)
  • Lower wingspan: 8.6 m (28 ft 3 in)
  • Height: 2.95 m (9 ft 8 in)
  • Wing area: 29 m2 (310 sq ft)
  • Empty weight: 820 kg (1,808 lb)
  • Gross weight: 1,240 kg (2,734 lb)
  • Powerplant: 1 ×Hiero 6 6-cylinder water-cooled in-line piston engines, 170 kW (230 hp)

Performance

  • Maximum speed: 175 km/h (109 mph, 94 kn)
  • Endurance: 3 hours 50 minutes
  • Service ceiling: 5,400 m (17,700 ft)
  • Time to altitude:
  • 1,000 m (3,281 ft): in 4 minutes 30 seconds
  • 2,000 m (6,562 ft): in 10 minutes 45 seconds
  • 3,000 m (9,843 ft): in 20 minutes 35 seconds
  • 4,000 m (13,123 ft): in 34 minutes 50 seconds
  • 5,000 m (16,404 ft): in 55 minutes

Armament
2 x 8 mmSchwarzlose machine guns (one synchronised forward-firing and one on a mount in rear cockpit)

References

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  1. ^abcdGrosz, Peter M.; George Haddow; Peter Schiemer (2002).Austro-Hungarian Army Aircraft of World War One. Boulder city: Flying Machine Press. pp. 109–114.ISBN 1-891268-05-8.
  2. ^abcdefgOrbis 1985, p. 2699

Bibliography

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External links

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Wikimedia Commons has media related toPhönix C.I.


KuKLFT C-class aircraft designations
Aviatik (Ö)
Hansa-Brandenburg
Knoller
Lloyd
Lohner
Oeffag
Phönix
Ufag
WKF
By role
Attack aircraft (A)
Bombers (B)
Army aeroplanes (Fpl)
Gliders2 (G/Lg/Se)
Helicopter2 (Hkp)
Fighters (J)
Advanced trainers (Ö)
Trials aircraft (P)
Reconnaissance (S)
Trainers (Sk)
Torpedo bombers (T)
Transports (Trp/Tp)
Post–1940
unified sequence
Italics Pre-unification designations  • 1 Assigned to multiple types  • 2 Not unified with main sequence
Authority control databases: NationalEdit this at Wikidata
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