Helmy Aerogypt

Helmy Aerogypt

__NOTOC__ Infobox Aircraft
name=Aerogypt


caption=
type=Four-seat cabin monoplane
national origin=United Kingdom
manufacturer=Helmy
designer=S Helmy
first flight=1939
introduced=
retired=1946
status=
primary user=
more users=
produced=1938
number built=1
variants with their own articles=
The Hemly Aerogypt was a British four-seat cabin monoplane designed and built by Egyptian S Helmy at Heston Aerodrome in 1938. The Aerogypt I was a low-wing cantilever monoplane powered initially by three 22hp (16kW) Douglas Sprite engines. The aircraft had an upward hinged roof which acted as a landing flap. Registered "G-AFFG" it first flew in 1939 and later had the hinged roof removed and was re-designated the Aerogypt II, another modification added end plates to the horizontal tail surfaces and was re-designated the Aerogypt III and last flown in that configuration in September 1940.

In 1943 the aircraft was modified as the Aerogypt IV with a tricycle landing gear and two 65hp (48kW) Continental A65 engines. It was damaged beyond repair after a landing accident in November 1946 at RAF Northolt when it was dropped by the recovery crane.

Variants

;Aerogypt I:Initial designation, a three-engine monoplane with tail wheel landing gear.;Aerogypt II:Modified with hinged roof removed.;Aerogypt III:Modified with end plates on horizontal tail surfaces.;Aerogypt IV:Rebuilt as a two-engine monoplane with tricycle landing gear.

pecifications (Aerogypt IV)

aerospecs
ref= [Jackson 1974, p 250]
met or eng?= eng

crew=1
capacity=3 passengers
length m=5.8
length ft=19
length in=0
span m=8.02
span ft=26
span in=4
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
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width m=
width ft=
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height m=
height ft=
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wing area sqm=
wing area sqft=
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=522
empty weight lb=1150
gross weight kg=1088
gross weight lb=2400
lift kg=
lift lb=

eng1 number=2
eng1 type=Continental A65
eng1 kw= 48
eng1 hp= 65
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
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max speed kmh=257
max speed mph=160
max speed mach=
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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=
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armament5=
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aircontent
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References

*cite book |last= Jackson|first= A.J.|authorlink= |coauthors= |title= British Civil Aircraft since 1919 Volume 3|year= 1974|publisher= Putnam|location= London|isbn=0 370 10014 X


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