Avia B.35

__NOTOC__ Infobox Aircraft
name=B.35


caption=
type=Fighter
manufacturer=Avia
designer=František Novotný
first flight=28 September 1938
introduced=
retired=
status=
primary user=
more users=
produced=
number built=3
variants with their own articles=The Avia B.35 (RLM designation Av-35) was a fighter aircraft built in Czechoslovakia shortly before World War II. It was designed to meet a 1935 requirement by the Czechoslovakian Air Force for a replacement for their B.534 fighter biplanes. The B.35 was an elegant, low-wing monoplane with a graceful elliptical wing. The fuselage was constructed from welded steel tube, covered in metal ahead of the cockpit and fabric aft, while the wing was of entirely wooden construction. Rather anachronistically, the Air Force specified fixed tailwheel undercarriage for the aircraft, in the hope that this would speed development.

Development

The first prototype, the B.35/1 displayed excellent flying characteristics and high speed and was originally powered by a Hispano-Suiza 12Ydrs piston engine. The powerplant was later changed to a Ycrs with identical power output, but with provision for an autocannon to be fitted between the cylinder banks to fire through the propeller hub. Testing continued until 22 November 1938, when the aircraft was destroyed in a crash that killed Avia test pilot Arnošt Kavalec. Nevertheless, a second prototype was already reaching completion, and was fitted with redesigned ailerons and flaps. It first flew on 30 December with testing beginning in earnest in February 1939. A pre-production series of ten aircraft was ordered, but before these could be built, Czechoslovakia was occupied by Germany in March.

Development resumed under German control, with the substantially revised B.35/3 flying in August 1939. The elliptical leading edges of the wings had been replaced with straight ones, and an outwardly-retracting main undercarriage fitted. This prototype was the first to actually carry its intended armament. Now, wearing German markings and registration "D-IPBB", it was displayed at the Salon de l'Aéronautique in Brussels, where enough interest was generated to spur development of an improved version of the aircraft as the B.135

Variants

* B-35/1 : First prototype.
* B-35/2 : Second prototype.
* B-35/3 : Third prototype.

pecifications (B.35/1)

aerospecs
met or eng?= met

crew=one pilot
capacity=
length m=8.50
length ft=27
length in=11
span m=10.85
span ft=35
span in=7
dia m=
dia ft=
dia in=
height m=2.60
height ft=8
height in=6
wing area sqm=17.00
wing area sqft=183
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=1,690
empty weight lb=3,726
gross weight kg=2,200
gross weight lb=4,850

eng1 number=1
eng1 type=Hispano-Suiza 12Ycrs
eng1 kw= 640
eng1 hp= 860
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=495
max speed mph=308
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=500
range miles=311
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=13.0
climb rate ftmin=2,560
sink rate ms=
sink rate ftmin=

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

References

Notes

Bibliography

* Bílý, Miroslav. "Avia B-35/B-135" (in Czech/English). Praha, Czech Republic: MBI, 2003. ISBN 80-86524-03-5.
* Green, William. "War Planes of the Second World War, Fighters, Volume One". London: Macdonald & Co.(Publishers) Ltd., 1960. ISBN 0-356-01445-2.
* Taylor, Michael J. H. "Jane's Encyclopedia of Aviation". London: Studio Editions, 1989.
* "World Aircraft Information Files". London: Bright Star Publishing. (pages=File 889 Sheet 85)

External links

See also

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