Junkers A 35

Infobox Aircraft
name=A 35


caption=
type=Postal, training and military aircraft
manufacturer=Junkers
designer=Mader and Zindel
first flight=
introduced=
retired=
status=
primary user=Russian Air Force
more users=
produced=
number built=186
unit cost=
developed from=
variants with their own articles=

Junkers A 35 was a two-seater cantilever monoplane, used for postal, training and military purposes. The aircraft was designed in the 1920s by Junkers in Germany and manufactured in Limhamn, Sweden and in Fili, Russia.

History

The A 35 was a development of a series of Junkers aircraft from 1918, starting with the J10/J11, the A 20, A 25, A 32, and finally the A 35. It was originally intended as a two-seat multi-purpose fighter aircraft and made its first flight in 1926. Due to the post-war restrictions, Hugo Junkers and the Soviet Government signed a contract about the setup of an aircraft facility at Fili in Russia in December 1922.

In 1926, the first Junkers L5 engines were mounted on the Junkers A 20s. With some further tail modifications the new aircraft was designated as A 35. A total of 24 aircraft were originally built as A 35s. A number of A 20s and A 25s were also modified with the Junkers L5 engine. The A 35 was also available with a BMW IV engine.

Versions

;Junkers A 20: The version manufactured in Limhamn was called R02 and the version manufactured in Fili was called Ju 20;Junkers A 20L:Landplane version.;Junkers A 20W:Floatplane version.;Junkers A 25: The version manufactured in Limhamn was called R41 and the version manufactured in Fili was called Type A;Junkers A 35: The version manufactured in Limhamn was called R53 and the version manufactured in Fili was called Type 20

Operators

*China as ROC (Junkers A-20)
*flag|Germany|Weimar
*USSR
*flag|Bulgaria

pecifications (A 35)

aircraft specifications

plane or copter?=plane
jet or prop?=prop

ref=Thulinista Hornettiin

crew=1
capacity=1
length main=8.22 m
length alt=26 ft 11 in
span main=15.94 m
span alt=52 ft 3 in
height main=3.50 m
height alt=11 ft 6 in
area main=29.76 m²
area alt= 320.2 ft²
airfoil=
empty weight main= kg
empty weight alt= lb
loaded weight main= kg
loaded weight alt= lb
useful load main= kg
useful load alt= kg
max takeoff weight main=1,600 kg
max takeoff weight alt= 3,520 lb
more general=

engine (prop)=Junkers L 5
type of prop=
number of props=1
power main=228 kW
power alt= 305 hp
power original= [ Given as 310 PS in original]

max speed main=206 km/h
max speed alt= 111 knots, 127 mph
cruise speed main= km/h
cruise speed alt= knots, mph
stall speed main= km/h
stall speed alt= knots, mph
never exceed speed main= km/h
never exceed speed alt= knots, mph
range main= km
range alt= nm, mi
ceiling main= m
ceiling alt= ft
climb rate main= m/s
climb rate alt= ft/min
loading main= kg/m²
loading alt= lb/ft²
thrust/weight=
power/mass main= W/kg
power/mass alt= hp/lb
more performance=
armament=
avionics=

Notes

ee also

aircontent
related=

similar aircraft=

sequence=

lists=
* List of military aircraft of Germany
see also=