Albatros C.X

Albatros C.X
	300px
	Scale model of k Albatros C.X

The Albatros C.X was a German military reconnaissance aircraft that saw service during World War I.

Design and development

The C.X was essentially an enlarged development of the Albatros C.VII designed to take advantage of the new Mercedes D.IVa engine that became available in 1917. Unlike the C.VII that preceded it in service, the C.X utilised the top wing spar-mounted radiator that had first been tried on the C.V/17. Other important modernisation features included provision for oxygen for the crew and radio equipment.

Operators

German Empire

Luftstreitkräfte

Specifications (C.X)

General characteristics

Crew: two, pilot and observer
Length: 9.15 m (30 ft 0 in)
Wingspan: 14.36 m (47 ft 1 in)
Height: 3.4 m (11 ft 2 in)
Wing area: 42.7 m² (459 ft²)
Empty weight: 1,050 kg (2,320 lb)
Gross weight: 1,668 kg (3,677 lb)
Powerplant: 1 × Mercedes D.IVa, 190 kW (260 hp)

Performance

Maximum speed: 175 km/h (110 mph)
Endurance: 3 hours 25 min
Service ceiling: 5,000 m (16,500 ft)
Rate of climb: 3.3 m/s (660 ft/min)

Armament

1 × forward-firing 7.92 mm (.312 in) Spandau LMG 08/15 machine gun
1 × 7.92 mm (.312 in) Parabellum MG14 machine gun for observer

References

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v t e World War I aircraft of the Central Powers
Fighters	AEG D.I AEG Dr.I Albatros D.I Albatros D.II Albatros D.III Albatros D.V Aviatik D.I Aviatik C.VI Daimler L.6 Euler D.I Euler D.II Fokker D.I Fokker D.II Fokker D.III Fokker D.IV Fokker D.V Fokker D.VI Fokker D.VII Fokker D.VIII Fokker Dr.I Fokker E.I Fokker E.II Fokker E.III Fokker E.IV Fokker E.V Halberstadt D.II Hannover CL.II Hannover CL.III Hannover CL.IV Hannover CL.V Hansa-Brandenburg W.12 Hansa-Brandenburg W.29 Junkers D.I Kondor D.6 Kondor E.III Naglo D.II Pfalz D.III Pfalz D.XII Pfalz Dr.I Pfalz E.I Pfalz E.II Phönix D.I LFG Roland D.II LFG Roland D.VI Siemens-Schuckert D.I Siemens-Schuckert D.II Siemens-Schuckert D.III Siemens-Schuckert D.IV Siemens-Schuckert L.I Zeppelin-Lindau D.I
Bombers and ground attack	AEG DJ.I AEG G.I AEG G.II AEG G.III AEG G.IV AEG G.V AEG J.I AEG J.II AEG R.I Friedrichshafen G.II Friedrichshafen G.III Gotha G.I Gotha G.II Gotha G.III Gotha G.IV Gotha G.V Gotha GL.VII Gotha G.IX Hannover CL.II Junkers CL.I Junkers J.I Rumpler G.I Rumpler G.II Rumpler G.III Zeppelin-Lindau Rs.II Zeppelin-Lindau Rs.III Zeppelin-Lindau Rs.IV Zeppelin-Staaken R.VI
Reconnaissance	AEG B.I AEG B.II AEG B.III AEG C.I AEG C.II AEG C.III AEG C.IV AEG C.V AEG C.VI AEG C.VII AEG C.VIII AGO C.I AGO C.II AGO C.III AGO C.IV AGO C.VII AGO C.VIII Albatros B.I Albatros B.II Albatros C.I Albatros C.III Albatros C.V Albatros C.VII Albatros C.IX Albatros C.X Albatros C.XII Aviatik B.I Aviatik B.II Aviatik C.I Aviatik C.VI DFW C.V LFG Roland C.II LVG B.I LVG C.II Rumpler C.I Rumpler C.IV Rumpler Taube
Trainers	Euler D.I
Prototypes	Albatros C.II Fokker V.1 Fokker V.2 Junkers J 1 Junkers J 2 Zeppelin-Lindau Rs.I

v t e Idflieg C-, CL-, CS-, and CLS-class aircraft designations
C- and CL-	AEG C.I C.II C.III C.IV C.V C.VI C.VII C.VIII AGO C.I C.II C.III C.IV C.VII C.VII Albatros C.I C.II C.III C.IV C.V C.VI C.VII C.VIII C.IX C.X C.XI C.XII C.XIII C.XIV C.XV Aviatik C.I C.II C.III C.V C.VI C.VIII C.IX BFW CL.I CL.II CL.III CL.IV DFW C.I C.II C.III C.IV C.V C.VI Fokker C.I Friedrichshafen C.I Germania C.I C.II C.IV Halberstadt C.I CL.II C.III CL.IV C.V C.VII C.VIII C.IX CLS.X Hannover C.I CL.II CL.III CL.IV CL.V Junkers CL.I LFG/Roland C.I C.II C.III C.V C.VIII LVG C.I C.II C.III C.IV C.V C.VI C.VIII OAW C.I C.II Otto C.I C.II Pfalz C.I Rumpler C.I C.III C.IV C.V C.VI C.VII C.VIII C.IX C.X Sablatnig C.I C.II C.III Schütte-Lanz C.I Zeppelin-Friedrichshafen C.I C.II Zeppelin-Lindau C.I C.II
CLS-	Albatros CLS.I Halberstadt CLS.I CLS.II (see also main sequence above) Junkers CLS.I
CS-	Zeppelin-Lindau CS.I

Albatros C.X

Contents

Design and development

Operators

Specifications (C.X)

References

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