Grahame-White Type X

Grahame-White Type X

__NOTOC__ Infobox Aircraft
name=Type X Charabanc


caption=
type=Five-seat passenger-carrying biplane
manufacturer=Grahame-White Aviation Company
designer=
first flight=1913
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=
The Grahame-White Type X Charabanc or Aerobus was an 1910s British passenger-carrying biplane designed and built by the Grahame-White Aviation Company based at Hendon Aerodrome, North London.

Development

To meet a demand for passenger-carrying flights that could not be satisfied by the earlier two-seat designs, the Grahame-White company designed a large passenger carrying biplane. It was an unuqual-span biplane of the boxkite type with a biplane tailunit with three rudders. It first flew in 1913 powered by a 120hp (89kW) Austro-Daimler engine and the aircraft was entered in the 1913 Michelin Cup. To meet the entry requirements it had to be an all-British aircraft so the engine was replaced with a British-built Green engine. The Charabanc went on to win the cup. To carry passengers the biplane had an elongated nacelle mounted on the lower wing for the pilot and four-passengers. It has been recorded that it once flew with a pilot and nine-passengers for nearly 20-minutes.

pecifications

aerospecs
ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1998
met or eng?= eng

crew=1
capacity=4 passengers
length m=11.43
length ft=37
length in=6
span m=19.05
span ft=62
span in=6
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=
height ft=
height in=
wing area sqm=73.39
wing area sqft=790
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=907
empty weight lb=2000
gross weight kg=1406
gross weight lb=3100
lift kg=
lift lb=

eng1 number=1
eng1 type=Green 6-cylinder inline piston
eng1 kw= 75
eng1 hp= 100
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=82
max speed mph=51
max speed mach=
cruise speed kmh= 72
cruise speed mph= 45
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=
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aircontent
see also=
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References

* The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1998


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