Wright Model C

Wright Model C

__NOTOC__ Infobox Aircraft
name=Model C


caption=
type=Scout
manufacturer=Wright Company
designer=
first flight=1912
introduced=
retired=
status=
primary user=
more users=
produced=
number built=8
variants with their own articles=
The Wright Model C was an early military aircraft produced in the United States and which first flew in 1912. It was a development of the Model B but was specifically designed to offer the United States Army a long-range scouting aircraft. It featured a more powerful engine over its predecessor, and an endurance of around four hours. Still a two-seater, it added a complete second set of controls, meaning that either crewmember could operate the aircraft. On some, the lever controls were replaced with two wheels mounted on a single yoke."United States Military Aircraft Since 1909" by F. G. Swanborough & Peter M. Bowers (Putnam New York, ISBN 085177816X) 1964, 596 pp.] Aerodynamically, the small finlets that had been used on the Model B's undercarriage were replaced by a double fin carried on an outrigger in front of the aircraft.

Seven Model Cs were delivered to the Army, serial numbers 7-8 & 10-14."United States Military Aircraft Since 1909" by F. G. Swanborough & Peter M. Bowers (Putnam New York, ISBN 085177816X) 1964, 596 pp.] They quickly earned themselves an unenviable reputation when six of the seven crashed within a short space of time, with the seventh aircraft deemed unairworthy and grounded. An eighth machine was built under licence by the Burgess Company as their Model J, Army serial number 18.

pecifications

aerospecs
met or eng?= eng

crew=One-two pilots
capacity=
length m=9.07
length ft=29
length in=9
span m=11.59
span ft=38
span in=0
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=2.24
height ft=7
height in=4
wing area sqm=40.9
wing area sqft=440
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=363
empty weight lb=800
gross weight kg=585
gross weight lb=1,290
lift kg=
lift lb=

eng1 number=1
eng1 type=Wright 6-cylinder water-cooled inline
eng1 kw= 56
eng1 hp= 75
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=100
max speed mph=60
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=
aircontent

related=

similar aircraft=

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see also=

References

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