Dayton-Wright Aerial Coupe

Dayton-Wright Aerial Coupe

__NOTOC__ Infobox Aircraft
name=OW.1 Aerial Coupe


caption=
type=three-seat touring aircraft
manufacturer=Dayton-Wright Company
designer=
first flight=1919
introduced=
retired=
status=
primary user=
more users=
produced=1919
number built=1
variants with their own articles=
The Dayton-Wright OW.1 Aerial Coupe was an American three-seat touring aircraft built by the Dayton-Wright Company of Dayton, Ohio. It was reputed to be the last aircraft designed by Orville Wright (hence the designation OW.1), but it relied heavily on the De Havilland DH.4 experience.

Following on from a wartime contract to build the British DH.4 under license, the Dayton-Wright Company looked at development of the aircraft for civil use. One of the aircraft designed was the OW.1 Aerial Coupe, still generally similar to the DH.4 configuration. It had lighter-weight wings, landing gear and tail unit. The main difference was a new fuselage to provide an enclosed cabin for a pilot and two passengers. The aircraft was powered by a Wright-Hispano inline engine located in the nose.

pecifications (OW.1)

aerospecs
ref= "The Illustrated Encyclopedia of Aircraft", (Part Work 1982-1985), Orbis Publishing, Page 1339
met or eng?= eng

crew=1 pilot
capacity=2 passengers
length m=8.69
length ft=28
length in=6
span m=14.02
span ft=46
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=2.74
height ft=9
height in=0
wing area sqm=49.61
wing area sqft=534
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=658
empty weight lb=1450
gross weight kg=1130
gross weight lb=2492
lift kg=
lift lb=

eng1 number=1
eng1 type=Wright-Hispano inline piston engine
eng1 kw= 134
eng1 hp= 180
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
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max speed kmh=153
max speed mph=95
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=805
range miles=500
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
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aircontent
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References

* "The Illustrated Encyclopedia of Aircraft", (Part Work 1982-1985), Orbis Publishing, Page 1339


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