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Junkers A 35
| A 35 | |
|---|---|
| Type | Postal, training and military aircraft |
| Manufacturer | Junkers |
| Designed by | Mader and Zindel |
| Primary user | Russian Air Force |
| Number built | 186 |
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
- Template:China as ROC (Junkers A-20)
- Template:Country data Germany
- Template:USSR
Specifications (A 35)
Data from Thulinista Hornettiin
General characteristics
- Crew: 1
- Capacity: 1
- Length: 8.22 m (26 ft 11 in)
- Wingspan: 15.94 m (52 ft 3 in)
- Height: 3.50 m (11 ft 6 in)
- Wing area: 29.76 m² (320.2 ft²)
- Empty weight: kg (lb)
- Loaded weight: kg (lb)
- Useful load: kg (kg)
- Max takeoff weight: 1,600 kg (3,520 lb)
- Powerplant: 1× Junkers L 5 , 228 kW (305 hp)[1]
Performance
- Never exceed speed: km/h (knots, mph)
- Maximum speed: 206 km/h (111 knots, 127 mph)
- Cruise speed: km/h (knots, mph)
- Stall speed: km/h (knots, mph)
- Range: km (nm, mi)
- Service ceiling: m (ft)
- Rate of climb: m/s (ft/min)
- Wing loading: kg/m² (lb/ft²)
- Power/mass: W/kg (hp/lb)
Notes
- ↑ Given as 310 PS in original
See also
Related lists
Lists relating to aviation | |
|---|---|
| General | Timeline of aviation · Aircraft · Aircraft manufacturers · Aircraft engines · Aircraft engine manufacturers · Airports · Airlines |
| Military | Air forces · Aircraft weapons · Missiles · Unmanned aerial vehicles (UAVs) · Experimental aircraft |
| Notable incidents and accidents | Military aviation · Airliners · General aviation · Famous aviation-related deaths |
| Records | Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft |
Lists relating to aviation | |
|---|---|
| General | Timeline of aviation · Aircraft · Aircraft manufacturers · Aircraft engines · Aircraft engine manufacturers · Airports · Airlines |
| Military | Air forces · Aircraft weapons · Missiles · Unmanned aerial vehicles (UAVs) · Experimental aircraft |
| Notable incidents and accidents | Military aviation · Airliners · General aviation · Famous aviation-related deaths |
| Records | Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft |
de:Junkers A 35 fi:Junkers A35
| This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Junkers A 35". |
