Focke-Wulf Fw 58
Focke-Wulf Fw 58 | |
---|---|
Type: | twin-engine trainer aircraft |
Design country: | |
Manufacturer: | |
First flight: |
January 18, 1935 |
Production time: |
until 1942 |
Number of pieces: |
1670 |
The Focke-Wulf Fw 58 " Weihe " was a twin-engine multi-purpose aircraft made by the Bremen manufacturer Focke-Wulf , which was primarily used as a training aircraft by the Air Force .
history
When the Luftwaffe was founded in 1935, an aircraft was needed for pilot training. Under the direction of chief designer Kurt Tank , Paul Klages and Andreas von Faehlmann developed a machine at Focke-Wulf, the dummy of which was available for inspection in February 1934. The Fw 58 V1 (D-ABEM, W.Nr. 451) flew for the first time on January 18, 1935. In June 1935, the V2 followed , which already had two arms.
The Fw 58 was able to assert itself against the somewhat smaller and with the same engines equipped rival development Arado Ar 77 , of which two copies were built. In Brazil , the license version Fw 58B-2 was produced with 25 machines.
Production numbers
Series production of the Fw 58 began in September 1936 and ended in August 1942.
version | FW | GFW | Miag | Luther | Gotha | total | comment |
---|---|---|---|---|---|---|---|
Test sample | 6th | 6th | V1 – V6, material no. 451, 452, 802, 1833, 1970, 1199 | ||||
B. | 307 | 88 | 395 | FW: versions B-1 and B-2, Miag: only version B-2 | |||
C. | 203 | 120 | 385 | 23 | 460 | 1191 | FW: versions C-1 and C-2, rest: only version C-2 |
Sales series | 76 | 76 | |||||
total | 592 | 120 | 473 | 23 | 460 | 1668 |
The following aircraft from the sales and RLM series were exported up to 1940: Argentina 3, Brazil 10, Bulgaria 8, Romania 22, Sweden 2, Turkey 6, Hungary 27, Austria 6. The following aircraft were delivered from 1942 to 1945: 10 Bulgaria, 5 Romania, 2 Sweden, 12 Slovakia, 202 Hungary.
use
The aircraft was used in various areas. The main purpose was the training of pilots for night flight and the training of bomb and machine gunnery.
In April 1938 Lufthansa bought four KJ-1 photo planes (W.-Nr. 2697-2700) for its daughter Hansa Luftbild. These aircraft were handed over to the RLM's special image department (SOBIA) at the start of the war. Between May and July 1939, DLH received five KL-1 cargo aircraft (W.-Nr. 3100-3104), two of which were passed on to the Brazilian subsidiary Syndicato Condor as PP-CBM (3102) and PP-CBN (3103). The aircraft were confiscated by the Brazilian Navy on November 18, 1942 and used as training aircraft. The D-OVXF (3104) crashed on January 24, 1942, killing the two-man crew. In order to set up its own airline "Slowenská Letecká Společnost", DLH delivered the last two Fw 58s to Slovakia in the course of the first half of 1942. DLH began air traffic with these aircraft on behalf of SLS, as there were probably no suitable personnel in Slovakia at the time. The aircraft received OK-TRE (3100) and OK-HLM (3101) certifications in July 1942. From 1943 the SLS then carried out the traffic with these aircraft itself.
In the Second World War (1939-1945) they were also used for light transport and ambulance flights as well as for surveying and weather reconnaissance flights.
From 1943, at the German Research Institute for Glider Flight (DFS) under the direction of Felix Kracht, an Fw 58 was successfully refueled by a four-engine Junkers Ju 90 during aerial refueling attempts in flight. However, due to a lack of fuel, one of the main problems faced by the German Air Force at the time, these attempts were stopped the following year.
construction
The Fw 58 was a twin-engine low - wing aircraft covered with fabric and metal . The landing gear was retractable. In the stern there was an open stand that could be equipped with an MG 15 (caliber 7.92 mm), another MG 15 could be mounted in the front of the fuselage.
The aircraft could also be equipped with skis and floats (Fw 58W).
Use as a test aircraft
One example (Fw 58 V14, D-OPDR) was extensively rebuilt and used for experiments with boundary layer suction. A better flow towards the tail unit should be achieved even at slower flight speeds. For this purpose, a Hirth aircraft engine was installed in the fuselage together with a fan with which the boundary layer on the trailing edge of the wing was extracted. This air then exited through two rows of circumferential slits in the rear part of the body.
Received aircraft
The only Fw 58 B-2 from Brazilian production that still exists today has the type designation AT-Fw 1530 and dates from 1941. The aircraft was flown at the Brazilian Força Aérea Brasileira , where it was in service until 1949. After that she found a new field of activity for a short time until 1955 at the Brazilian Ministry of Agriculture with the label PP-FDE.
Encounter with the Supermarine Spitfire
In November 1941 Kurt Tank and other employees of the Focke-Wulf design office flew back to Bremen in the unarmed Fw 58 A-0 (D-ALEX) after a meeting at the French aircraft manufacturer SNCASO . In the Brussels area they met two British Supermarine Spitfires . Although the British shot past in the first attack, whereupon Tank tried to escape at low altitude, the second attack ended with a badly damaged left wing and a torn off aileron, which meant that the machine could only be controlled to a very limited extent. The fighter pilots left the obviously unarmed, slow and easy prey alone. After 17 anxious minutes, Tank flew the machine with the remaining ailerons in the next place near Hilversum, southeast of Amsterdam. The crew left the machine, which was damaged with 47 bullet holes, unharmed - a bullet stuck in the tanks' seat cushions. To the astonishment of the staff at the Focke-Wulf design office, the next morning the aircraft was ready to fly - the Air Force mechanics repaired the aircraft in just seven hours.
Military users
- Argentina : 1938–1952
- Brazil : Manufacturing under license
- Bulgaria
- German Empire
- Finland
- Croatia
- Netherlands
- Austria ( Air Force )
- Poland
- Romania
- Sweden
- Soviet Union
- Czechoslovakia
- Turkey
- Hungary : license production
Technical specifications
Parameter | Fw 58 B-1 | Fw 58 B-2 | Fw 58 C-2 | Fw 58 V13 (from 1942: KL-1) |
---|---|---|---|---|
Usage | Trainer aircraft | Machine-gun and bomb-dropping training aircraft | Blind flight and FT trainer aircraft | Feeder and airliner |
crew | Pilot, radio operator + max. 4 people | 4 (pilot, bombardier, machine gunner and radio operator) | 2 | |
Drive: 8-cylinder V-engine | 2 × Argus As 10 C, air-cooled, hanging, each 240 PS (approx. 180 kW) | 2 × Hirth HM 508 DB, air-cooled, suspended installation, each 280 PS (approx. 210 kW) | ||
length | 14.0 m | 14.16 m | 14.00 m | |
span | 21.0 m | 21.05 m | ||
height | 4.30 m | 4.20 m | 4.25 m | 3.90 m |
Gauge | 4.00 m | |||
Wing area | 47 m² | 47.30 m² | 47.00 m² | |
V shape | 7.5 ° | |||
Arrow shape | 12.5 ° | |||
Wing loading | 62.5 kg / m² | 76.55 kg / m² | ||
Breaking load multiple | 6.2 | 5.45 | ||
Empty mass | 1900 kg | 2000 kg | 1960 kg | 2400 kg |
Preparation mass | 2300 kg | 2000 kg | 2500 kg | |
Payload | 630 kg | 640 kg | 1080 kg | |
Takeoff mass | 2810 kg | 2930 kg | 2926 kg | 3600 kg |
Top speed | 256 km / h | 254 km / h at 0 m and 222 km / h at 4000 m | 265 km / h at 0 m and 231 km / h at 4000 m | 272 km / h at 0 m |
Marching speed | 238 km / h in 0 m and 218 km / h in 3000 m | 249 km / h in 0 m and 227 km / h in 3000 m | 242 km / h at 0 m | |
Landing speed | 76 km / h | 85 km / h | ||
Takeoff route | approx. 200 m | |||
Landing route | approx. 180 m | |||
Climb performance | 1000 m in 3.8 min 2000 m in 8.5 min 3000 m in 14.5 min 4000 m in 22.9 min 4.7 m / s near the ground |
1000 m in 3.7 min 2000 m in 8.3 min 3000 m in 14 min 4000 m in 22 min 4.9 m / s near the ground |
5.0 m / s near the ground | |
Flight duration | approx. 3.3 h | approx. 5 h | 3.6-6.7 h | |
Range | 676 km | approx. 610 km | 1080 km | 800-1500 km |
Service ceiling | 5200 m | 5400 m | 5600 m | 5400 m |
Single-engine hovering height | 2000 m | 1000 m | ||
Armament | 2 × MG 15 (7.92 mm) | 2 × MG 15 (7.92 mm) (possible in A and B stand) | - |
See also
literature
- Karl R. Pawlas: Aviation Lexicon. Entry ID: 3120-100-1
- Rudolf Höfling: The last consecration . In: Flugzeug Classic . No. 8 , 2006, ISSN 1617-0725 , p. 24-29 .
- The magazine for aviation, contemporary history and oldtimers: Airplane Classics Special 7. 2011, instructor "Weihe"
Web links
Individual evidence
- ↑ According to the company tradition of that time, all Focke-Wulf aircraft had internal bird names.
- ↑ René Scheer: Paul Klages: In the shadow of Kurt Tanks . In: Aviation Classics . No. 6/2015 . Motor Presse, Stuttgart, p. 54 .
- ^ Documents from the Federal Archives / Freiburg Military Archives, holdings RL 3
- ↑ Luftfahrt International 1, p. 14 ff.
- ^ Documents from the Lufthansa archive, Cologne
- ↑ P 6 - Focke Wulf Fw 58C-2 "Weihe" (1938–1959)