U.S. Air Service |
AIRCRAFT
OF THE
A E F
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Caudron G.IV
Development and Operation
The Caudron G.IV was produced in response to an Aviation Militaire request for a more powerful Army Coordination aircraft capable of carrying a forward firing machine gun. The aircraft was a revision to the Caudron G.III. A second engine was added and the central nacelle was lengthened to allow for a nose gunner, and the number of rudders was increased from two to four. The armament consisted of a 7mm Hotchkiss or Lewis gun on a flexible mounting. The aircraft first flew in March 1915.
The United States Air Service of the A.E.F. purchased ten Caudron G.IV's for use as trainers at Tours. American cadets undergoing flight training at Tours leading to assignment as Army cooperation/reconnaissance/bombing pilots trained on this machine.
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Aircraft and Flight Characteristics
Caudron G.IV 2-seat reconnaissance aircraft with two 80 hp Le Rhône engines
Length
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7.19 m
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Height
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2.55 m
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Empty Weight
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733 kg
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Loaded Weight
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1232 kg
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Maximum Speed
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At Sea Level
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130 km/hr
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At 2000 m
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125 km/hr.
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Wing Span
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16.85 m |
Climb
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To 1,000 m
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6 minutes 30 seconds
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To 2,000 m
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15 minutes
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Endurance
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5 hrs.
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Payload
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210 kg.
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Armament
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One nose-mounted 7-mm Hotchkiss or Lewis machine gun. Crew was also equipped with a carbine or a Chauchat gun
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References:
- Davilla, J. and Art Soltan, French Aircraft of the First World War
- Photo from the author.
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Great War Society
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