Focke-Wulf Fw-189 Uhu

Fw-189A

The Focke-Wulf Fw 189 was designed in response to the German Air Ministry specification issued in February 1937. This called for an aircraft with a crew of three and better performance than the Hs 126, then about to enter service as the standard reconnaissance aircraft.

Arado, Blohm und Voss and Focke Wulf each produced a design in response to this specification. To meet this specification, Focke Wulf’s team under the leadership of Kurt Tank evolved a twin boom design. A 430 hp Argus As 410 12-cylinder air cooled inverted V type engine was installed at the front of each slender tail boom, driving a two blade propeller, and mounted on the centre section of the wing, between the booms, was an extremely well glazed nacelle accommodating the three man crew. Each tail boom terminated in a single fin and rudder, bridged by a centrally mounted tailplane.

The first prototype, the Fw 189 V1 (registration D-OPVN), made its maiden flight in July 1938. No armament was fitted to the Fw 189 V1, but the second prototype (D-OVHD), which flew in August 1938, was armed with a 7.9 mm (0.311 in) MG 17 machine gun in each wing root and three 7.9 mm MG 15 guns: one each in the nose, a dorsal blister, and the tailcone of the nacelle. The V3 (D-ORMH) was unarmed, but had the definitive 450 hp As 410-1A engines intended for production aircraft and automatic variable pitch propellers.

The success of the first three prototypes was rewarded with an order for a second series of four prototypes. The Fw 189 V4 fourth prototype was representative of the Fw 189A production configuration, but it was actually the Fw 189B, based on the V5, that was first to be ordered into production by the RLM in 1939. V4 had modified engine cowling, semi-cowled main wheels, a larger main wheels and only two machine guns. The wing root guns remained, as did the upper and rear pod guns, although the front gun was removed. The V4 was used for tests with smoke-screen equipment and with equipment for using poisoned gas and chemical weapons. V5 was the prototype for the B series of training aircraft. V6 was the prototype for the planned series of heavily armoured ground attack aircraft and V7 was to be built as a prototype of a twin-float version of the aircraft, although it was completed as one of three B-0 trainers.The Fw 189B (three B-0s and ten B-1s) was built as an unarmed, dual control five seat trainer, its modified nacelle lacking the nose and tailcone glazing of the A series prototypes.

Production of the Fw 189A finally got under way in the spring of 1940, a batch of ten pre-production Fw 189A-0s for service trials being followed by the first series version, the Fw 189A-1. In the spring of 1940 Focke-Wulfe received an order for ten pre-production A-0s and twenty A-1s. The A-1 was armed with two fixed forward firing MG 17s and two flexibly mounted MG 15s. The first of these was carried in a circular glass turret on the roof of the cockpit, while the second was mounted in the conical rear cone of the pod, which could rotate through 360 degrees. The A-1 could also carry four 154lb/ 75kg bombs and an RB 20/30 camera as standard, with a wide range of other cameras available. Large scale production didn’t get under way until late in 1940. This began to reach Luftwaffe units in late 1940 and early 1941, and eventually equipped at least nine Aufklarungsgruppen (long range reconnaissance wings) and 15 Nahaufklarungsgruppen (short range reconnaissance wings), most of them on the Eastern Front. Known variously as the Uhu (owl), or as das Fliegende Auge (the flying eye) of the Wehrmacht.

Production Fw 189A-1s carried an armament similar to that of the second prototype, except that the nose machine gun was deleted. The second production version, the Fw 189A 2, differed in having 7.9 mm (0.311 in) MG 81Z (twin MG 81) guns in the dorsal and tailcone positions, instead of the MG 15s. The Fw 189A4 (the Fw 189A-3 was an unarmed trainer) was a ground support development of the A-2, having ventral armour plating and 20 mm (0.79 in) MG FF cannon instead of MG 17s in the wing roots. All except the A- 3 could carry four 50 kg (110 lb) bombs on racks under the outer wings. The Fw 189A-1/Trop was a hot climate version for service in the Mediterranean and North African theatres; the A-1/U2 and A-1/U3 were two special one off conversions for a VIP transport role; the single Fw 189E was another A-1, converted to 700 hp French Gnome Rhone 14M radial engines; and many A types were, in their later years, used for such secondary duties as liaison and casualty evacuation. Some even had a short spell as night fighters with I/NJG 100. A number of were purpose-built five-seat trainers.

The Fw 189 was given a high production priority and was produced at several factories across Europe, with new production lines being established in Prague and around Bordeaux although production began at Focke-Wulf’s own factory at Bremen. The type became the main German tactical reconnaissance aircraft from 1942 until the summer of 1944. Thirty eight aircraft were delivered by the end of 1940, sixty-one in 1941, fifty seven in 1942 and eleven in 1943. By this point production was being concentrated around Bordeaux, while the Bremen factory was focusing on the Fw 190. The second production line was in the Aero-Avia factory at Prague. This factory produced 151 aircraft in 1940-41, 183 in 1942 and three in 1943, for a total of 337. The final production line was set up around Bordeaux. At first the French factories assembled aircraft from German-built sub-assemblies, completing 87 aircraft in 1942. In 1943 the French factories were responsible for most remaining aircraft, before production of the Fw 189 was cancelled early in 1944. Eventually 864 Fw 189s were completed, 337 at Prague, between 250 and 300 in France (sources differ, and sub-totals often don’t add up), and the rest at Bremen. Production reached its peak in 1942.

At the start of the war German short range reconnaissance was carried out by squadrons designated as Aufklärungsstaffeln (Heer), abbreviated to Aufkl.(H) or (H). Thirty six such squadrons existed in August 1939, and were under army control. Each squadron was self-supporting and fully mobile and could move from location to location under its own steam. The first few Fw 189s reached experimental sections of the Luftwaffe in the spring of 1940. At about the same time some aircraft reached the reconnaissance squadrons for service trials, but large-scale deliveries didn’t really begin until the end of 1942. On 22 July 1941, at the start of the invasion of the Soviet Union, the number of reconnaissance squadrons had risen to 54, most of which were still using the Hs 126. Production of the Fw 189 increased in pace during the year, but even at the end of 1942 the Hs 126 still made up a significant proportion of the available aircraft. In the winter of 1941-42 the squadrons were organised into short-range reconnaissance groups, each of which was meant to contain three squadrons. On the southern sector there were nine groups with sixteen squadrons, of which six were still using the Hs 126. In the middle sector things were worse, with six groups and thirteen squadrons, of which nine still had the Hs 126. Finally both squadrons operating in the north were still using the older aircraft. Of a total of 31 short-range reconnaissance squadrons, 17, or just over half, were still using the older aircraft. By the summer of 1944 the Fw 189 had been forced out of the daytime skies, and the surviving aircraft were forced to operate at night, or as training and liaison.

In April 1937 Focke-Wulf received a contract to produce a single prototype, which made its maiden flight in July 1938 and it was this prototype that was evaluated by the Ilmavoimat / Maavoimat / VL team in August of the same year.

The Ilmavoimat viewed the Fw 189 as a rugged and simple aircraft to be used solely for short-range tactical reconnaissance and coordinating close air support and artillery strikes with forward ground operations. The intention was to operate the aircraft from rough forward air bases and for the aircraft to have a higher maximum speed than the Fi 156. It was also intended that the aircraft be used for front-line low-level reconnaissance and aerial photography. This aircraft had rated very highly in the evaluations, with excellent all-round visibility, good stability and responsiveness and able to maintain steady flight on one engine as well as being exceptionally agile and strongly constructed. The layout and positioning of navigational equipment and radios was carefully thought out, cockpit heating was efficient and it was easy to put the aircraft on target when laying down marker bombs.

The Ilmavoimat ordered twenty of the Focke Wulf Fw 189’s. There were some design modifications specified. The pilot and observer/controller were to sit side by side, making communications easy. Armour was added under the fuselage and engines and self-sealing fuel tanks were specified. Armament consisted of two machine guns on a flexible mount in a dorsal position and four fixed machine guns in the wing roots, firing forwards. After delivery, two Hispano-Suiza 404 20mm cannon were fitted in a blister beneath the fuselage. The rear gunner position of the German-version was eliminated to reduce weight and rather than 4 hardpoints for 50kg bombs, 8 hardpoints for 30kg phosphorus marker bombs were fitted. The aircraft was just entering production in Germany and with the German eager for hard currency, the Ilmavoimat got the first twenty aircraft of the German production lines, perhaps unfortunately as Focke Wulf used these to iron out some of their initial production line problems. Despite this, the Ilmavoimat found the Fw 189’s to be a superb front line reconnaissance aircraft, tough and durable, able to take a lot of damage and maneuverable enough to stay out of trouble even if caught on it’s own.

Fw 189 cockpit

The Ilmavoimat’s Fw 189’s were delivered in February 1939, much to the relief of the High Command, who were unsure which orders that had been placed would actually be fulfilled up until the moment that the aircraft actually arrived in Finland. To this end, after the Munich Crisis, and as part of Finland’s emergenmcy measures, it was specified that wherever possible, Finnish military equipment purchases would be carried on Finnish cargo ships wherever feasible, even if this meant additional shipping costs. After the Munich Crisis, as Finland experienced what would in later years be called “The Great Awakening,” a wide range of emergency measures were put in place and additional emergency funding for military equipment was provided. Among this funding was provision for a further twenty Fw 189’s. These were ordered in December 1939 and to the relief of the Ilmavoimat, actually delivered in May 1939. With tensions increasing with the Soviet Union, a further order was placed for forty Fw 189’s in July 1939, but this was cancelled by the German government on the 19th of August 1939, shortly after Molotov Ribbentrop Pact was signed.

Slovakia, a nominally independent republic which came into being following the Nazi dismemberment of Czechoslovakia, received 14 Fw 189A and Hungary about 30 A-2s.

Production ended in August 1944, by which time a total of 864 Fw 189s had been completed. Of these, 310 were produced by the SNCA du Sud Ouest at Bordeaux Merignac during 1942 44 and 337 Fw 189As by the Aero factory in Czechoslovakia between 1941 43.

The French total comprised 293 Fw 189As plus 17 examples of the Fw 189F 1, a version of the A 2 with 580 hp Argus As 411MA- 1 engines. Focke Wulfs total of 217 included six prototypes, 198 Fw 189As and 13 Fw 189Bs. The sixth prototype (V6) and modified first prototype (Vlb) were used flight test a very much smaller, well armoured two seat nacelle intended for the proposed Fw 189C assault version: other projects that did not come to fruition were the twin float Fw 189D and the 950 hp 402 engined Fw 189G.

Gallery

Fw 189A-1
Engines: 2 x Argus As 410A-1, 347kW / 459 hp
Wingspan: 18.4 m / 60 ft 4 in
Length: 12.03 m / 39 ft 6 in
Height: 3.1 m / 10 ft 2 in
Wing area: 38.0 sq.m / 409.03 sq ft
Max take-off weight: 3950 kg / 8708 lb
Empty weight: 2805 kg / 6184 lb
Wing load : 21.32 lb/sq.ft / 104.0 kg/sq.m
Max. speed: 181 kts / 335 km/h / 208 mph
Cruise speed: 170 kts / 315 km/h / 196 mph
Service Ceiling: 7000 m / 22950 ft
Range: 362 nm / 670 km / 416 miles
Crew: 2-3
Armament: 2x MG 15 7,92mm, 2x MG 17 7,92mm, 4x 50kg Bomb.

Fw 189A 2
Engines: 2 x Argus As.410 A-1, 347kW / 459 hp.
Span: 18.40 m (60 ft 4.5 in)
Length: 12 m (39 ft 4.5 in)
Gross weight: 3950 kg (8710 lb).
Maximum speed: 350 km/h (217 mph).

Focke-Wulf Fw-187 Falke

The Fw 187 was a heavy, single-seat, twin-engined fighter. Despite very good performance, the Luftwaffe showed no interest, as it was firmly committed to the Bf 110. Nine were built in total.

The first was destroyed in an accident on 14/05/1938. The third prototype featured a fuselage remodel and engine nacelles redesign and flew in 1938.

Fw 187 V 1
Engines: 2 x Junkers Jumo 210Da, 630 hp
Props: three-bladed metal Junker-Hamilton
Wingspan: 15,30 m
Length: 11,10 m
Height: 3,85 m
Wingarea: 30,40 sq.m
Vmax: 525 kph
Seats: 1
Armament: 2 x MT MG 17 7,92 mm
1st prototype, D-AANA

Fw 187 V 2
Engines: 2 x Junkers Jumo 210G, 680 hp
Props: three-bladed metal VDM fixed pitch
Wingspan: 15,30 m
Length: 11,10 m
Height: 3,85 m
Wingarea: 30,40 sq.m
Vmax: 525 kph
Seats: 2
Armament: 6 x MT MG 17 7,92mm
First flown: 1937
D-ORHP.

Fw 187 V 3
Seats: 2
Armament: 2 x MG FF 20mm

Fw 187 V-4
Engines: 2 x Junkers Jumo 210G, 680 hp
Props: three-bladed metal VDM fixed pitch
Wingspan: 15,30 m
Length: 11,10 m
Height: 3,85 m
Wingarea: 30,40 sq.m
Vmax: 525 kph
Seats: 2
Armament: 6 x MT MG 17 7,92mm

Fw 187 V-5
Engines: 2 x Junkers Jumo 210G, 680 hp
Props: three-bladed metal VDM fixed pitch
Wingspan: 15,30 m
Length: 11,10 m
Height: 3,85 m
Wingarea: 30,40 sq.m
Vmax: 525 kph
Seats: 2
Armament: 6 x MT MG 17 7,92mm

Fw 187 V-6
Engines: 2 x Daimler-Benz DB 600A, 1075 hp
Props: three-bladed metal VDM fixed pitch
Wingspan: 15,30 m
Length: 11,10 m
Height: 3,85 m
Wingarea: 30,40 sq.m
Vmax: 630 kph
Seats: 2
Armament: 6 x MT MG 17 7,92mm

Fw 187 To 0
Engines: 2 x Junkers Jumo 210G, 680
Props: metal VDM fixed pitch
Wingspan: 15,30 m
Length: 11,10 m
Height: 3,85 m
Wing area: 30,40 sq.m
Empty weight: 3700 kg
MTOW: 5000 kg
Vmax: 525 kph @ 4000 m
ROC: 2000 m in 1 min
Ceiling: 10000 m
Armament: 4 x MT MG 17 of 7,92mm and 2 guns 20 mm.
Number built: 3

Focke-Wulf Fw-159

The Fw 159 was a parasol-wing fighter with retractable landing gear, competing with the Messerschmitt Bf 109. Three were built, the first flying in 1935. They suffered from serious problems with their landing gear, the second prototype being reinforced.

V 1
Engine:
Junkers Jumo 210A, 610 hp
Prop: metal three-bladed variable pitch
Wingspan: 12,40 m
Length: 10,00 m
Height: 3,75 m
Wingarea: 20,20 sq.m
Empty weight: 1875 kg
MTOW: 2250 kg
Power loading: 111,38 kg/sq.m
Power loading: 3,688 kg/hp
Vmax: 385 km/h
Ceiling: 7200 m
Range: 650 km
Armament: 2 MT MG 17, 7.92 mm.

V 2
Engine: Junkers Jumo 210B, 640 hp
Prop: Schwartz two-blade wood variable pitch
Wingspan: 12,40 m
Length: 10,00 m
Height: 3,75 m
Wingarea: 20,20 sq.m
Empty weight: 1875 kg
MTOW: 2250 kg
Wing loading: 111,38 kg/sq.m
Power loading: 3,515 kg/hp
Vmax: 333 kph @ SL, 370 kph @ 1500 m, 385 kph @ 4000 m
Vcruise: 365 kph @ 2700 m
ROC: 6000 m in 12 min 30 sec
Ceiling: 7200 m
Range: 650 km
Armament: 2 MT MG 17 7,92 mm

V 3
Engine: Junkers Jumo 210G, 730 hp
Vmax: 405 kph @ 4500 m.

Focke-Wulf Fw-58 Weihe / Oficinas Gerais da Aviation Naval Fw 58B-2

The Weihe was first flown in prototype form in 1935 as an advanced training, light 6 passenger transport and communications aircraft for the Luftwaffe, powered by two 179kW Argus As.10G engines. The main undercarriage retactable, and tail wheel fixed.

Before the outbreak of World War II Deutsche Luft-Hansa received eight as six-passenger commercial transports. Armament in the military training version comprised a gunner’s turret in the nose (which could be replaced by a metal cone for blind-flying instruction) and an aft gun position. The turret had space for an instructor and pupil for machine-gun and bomb-aiming training. Two seats side-by-side were provided in the cockpit for flying training, while a bomb trap with sights in a further compartment was provided for bombing instruction.

Fifteen were licence built by Brazil’s Oficinas Gerais da Aviation Naval during 1939-40. These were based on the Fw 58B-2 which was used as a gunnery trainer by the Luftwaffe.

Total production: 1350

V-1
Engines: 2 x Argus Ace 10c, 240 hp
Props: two-blade metal fixed pitch
Wingspan: 21,00 m
Length: 14,00 m
Height: 3,90 m
1 prototype

V-2:
Armament: 1 MT MG 15 7,92 mm, 1 MT MG 15, 7,92 m
1 prototype.

V-4:
Armament: 1 MT MG 15 7,92mm
1 prototype

Fw 58B-1
Engines: 2 x Argus Aces 10c, 240 hp
Props: two-blade wood variable pitch
Wingspan: 21,00 m
Length: 14,00 m
Height: 3,90 m
Wingarea: 47,00 sq.m
Empty weight: 2400 kg
MTOW: 3600 kg
Wing loading: 76,595 kg/sq.m
Power loading: 7,5 kg/hp
Vmax: 270 kph
Vcruise: 240 kph
Ceiling: 5600 m
Range: 800 km
Armament: 2 x MT MG 15, 7,92 mm

Fw 58B-2

Fw 58C
Engines: Argus Ace 10c or Hirth HM 508D, 260 hp

Fw 58W
Undercarriage: two catamaran floats

Focke-Wulf Fw-57

A twin-engined, three-seat strategic fighter, first flown in 1936. The Fw 57 was a contemporary of the Bf 110, with which it competed for orders. It featured a powered dorsal gun turret, and a glazed nose with twin semi-flexible cannon operated by the third crewmember. The Fw 57 was overweight and underpowered. Only three were built.

Fw 57
Engines: 2 x Daimler-Benz DB 600-A, 910 hp
Props: metal three-blade fixed pitch
Wing span: 25,00 m
Length: 16,40 m
Height: 4,08 m
Empty weight: 6800 kg
MTOW: 8300 kg
Vmax: 404 kph
Ceiling: 9100 m
Armament: 2 x MG FF, 20 mm (nose) and 1 Mauser MG FF, 20 mm (dorsal turret).

Focke-Wulf Fw-56 Stosser

The Stosser (hawk) was the first Focke-Wulf design undertaken by Kurt Tank, and resulted for a German requirement for an advanced trainer with the As 100 engine. The resultant Fw 56 prototype that flew in November 1933 was a parasol-winged aeroplane of mixed construction with cantilever main landing gear units powered by a 179kW Argus As. 10C engine: two more prototypes followed. The V2 prototype had a modified undercarriage and metal wing. The V3 prototype had a further modified undercarriage, similar to the V1, first flying in 1934.
Three Fw 56 A-0 were built with various modifications to the aerofoil. Two MT MG 17 of 7,92 m/m were fitted and provision for 3 bombs of 10 kg.
In the summer of 1935 the Stosser was selected in preference to the Arado Ar 76 and Heinkel He 74, so three Fw 56A-0 pre-production and about 900 Fw 56A-1 production aircraft followed up to the end of production in 1940. These were extensively used as advanced trainers in fighter schools, though after trials that helped to validate the concept of dive-bombing the type was also used in dive-bomber schools. Austria ordered the type before its annexation by Germany, and 12 Stossers were also delivered to Hungary.

Fw 56 V1
Engine: Argus As 10C, 240 hp
Prop: 2 blade fixed pitch
Seats: 2
1 prototype

Fw 56 V2
1 prototype

Fw 56 V3
1 prototype

Fw 56 A-0
Armament: 2 MT MG 17 7,92 mm / 3 bombs 10 kg

Fw 56 A-1 Stosser
Engine: Argus Aces 10c, 240 hp / 179kW
Prop: two-bladed variable pitch
Wingspan: 10,50 m (34ft 5.5 in)
Length: 7,70 m (25ft3in).
Height: 3,55 m
Wingarea: 150.696 sq.ft / 14 sq.m
Empty weight; 695 kg
MTOW: 995 kg
Max. payload weight : 145.5 lb / 66.0 kg
Fuel capacity: 22 gal / 84 l
Vmax: 173 mph / 278 kph @ SL
Landing speed: 49 kt / 90 km/h
Cruising speed : 132 kt / 245 km/h
Take off distance: 551 ft / 168 m
Initial climb rate : 1496.06 ft/min / 7.6 m/s
Service ceiling : 20341 ft / 6200 m
Range: 400 km / 249 miles
Crew: 1
Armament: 1 or 2 Mg 17, 7,92mm plus provision for 3 x 10-kg (22-lb) bombs carried externally.

Focke-Wulf A-47

Developed to meet the requirements of the German meteorological service, the two seat, open cockpit prototype Focke-Wulf A 47 weather reconnaissance aircraft was first flown in June 1931 by Cornelius Edzard. Powered by a 164kW Argus As 10 engine, the A 47 was a parasol-wing monoplane with a wing of wood construction and a fabric-covered steel-tube fuselage. It was tested extensively by the Reichsverband der Deutschen Luftfahrtindustrie (predecessor of the present BDLI, or Federation of the German Aerospace Industries) and then evaluated operationally at the Hamburg weather centre, beginning in December 1932. Successful completion of the programme led to production orders, delivered between 1934 and 1936, and used by the meteorological service all over Germany.

Engine: Argus Aces 10, 220 hp
Prop: two-blade variable pitch 2,80 m diameter
Wingspan: 17,76 m
Length: 10,50 m
Height: 3,04 m
Wingarea: 35,00 sq.m
Empty weight: 950 kg
MTOW: 1475 kg
Fuel: 2x 75 lt
Wing loading: 42,142 kg/sq.m
Pwr loading: 6,704 kg/hp
Vmax: 172 km/h
Stall: 77 km/h
ROC: 1000 m in 6 min, 2000 m in 13,3 min, 4000 m in 34 min

Focke-Wulf F.19 Ente

Focke-Wulf F 19a “Ente”

Focke Wulf Flugzeugbau G.m.b.H. built a twin engined canard in 1927. They called it the F.19 Ente, claiming that the tail first configuration gave it ‘exceptional stability and control at low speeds’. Stability and control in slow flight means safety.

Georg Wulf was killed September 29, 1927 test-flying an F-19 Ente canard.