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History Brief, by Dave Simpson, edited by Johan Visschedijk

April 14, 2004

Focke-Wulf Fw 187 Falke "Falcon"


First designed in 1935 by Kurt Tank with absolutely no official requirement, the single seat design was conceived at around the same time as the Westland P.9 (later Whirlwind) and Lockheed 22 (later XP-38 Lightning).

The initial design performance calculations showed a potential speed of 348 mph (560 kmh) using 860 hp Daimler-Benz DB 600 engines. The design and specifications were unveiled in 1936 at an exhibition of new weapons, prototypes and projects held at Berlin-Schonefeld. The appraisal of high ranking party members, government officials and service personnel was such that why waste two engines on a fighter when one engine was more than sufficient for a single seat fighter... The common "wisdom" of the day was that a long-range escort fighter was just not needed as the bombers had sufficient speed and defences to not need an escort in order to achieve their tactical duties.

Kurt Tank after this exhibition took his design directly to Oberst Wolram von Richtofen, chief of the development section of the Techischem Amt. He had the foresight to know that air warfare was a technological battle, and fighters would soon be designed and built faster and better armed. He authorized a development contract for three prototype Fw 187 fighters (V1-V3). Interestingly von Richtofen's tenure at this post was destined to be brief... one can only speculate on how the war would have turned out if some of the designs for strategic bombers, jet fighters and rocket interceptors had not been ignored in the late 1930s.

The first prototype Fw 187 V1 (D-AANA) was ready to fly in spring 1937, and was powered by two 680 hp Jumo 210Da engines. Even with these low powered engines the aircraft attained 326 mph (525 kmh) at 13,123 ft (4,000 m), a full 50 mph (80 kmh) faster than the latest Bf-109B-2 production single-seat fighters.

The aircraft was lost on May 14, 1938 during a low level high-speed pass at the test facility in Bremen. The pilot was believed to have pulled up to sharply at the end of the pass, the aircraft stalled, and spun into the ground.

The second prototype Fw 187 V2 was flying by summer of 1937 and it was destined to be the last single seat version. Earnst Udet had replaced von Richtofen by this point in time, and while Udet was a visionary in some respects, he was a total conventionalist when it came to fighter planes. Two engined fighter planes were less maneuverable than single seat fighters so all further development of the Fw 187 was to be as a "Zerstorer" (destroyer) having two or three seats and heavy armaments for attack and defence. History later showed that this category, (Bf-110 day fighters) to be totally out classed by modern monoplane single seat fighters in daylight encounters...

The third prototype Fw 187 was radically altered, but to save weight and dimensional changes the extra position was as a radio operator with no defensive guns. This third Fw 187 V3 (D-ORHP) flew in spring 1938 and had a short troubled career. It suffered a starboard engine fire during one of the initial test flights culminating in a landing that damaged both main landing gear.

The next two prototypes Fw 187 V4 (D-OSNP) and V5 (D-OTGN), completed summer and autumn 1938 respectively, were built as two seaters. Both airframes were powered by Jumo 210Da engines and while both received sufficiently favorable flight test results, the top speed achieved was less than expected.

The next prototype Fw 187 V6 (CI-NY) was able to utilize two 1000 hp Daimler-Benz DB 600A liquid cooled engines and was outfitted with surface evaporation cooling to reduce the drag of coolant radiators. While Kurt Tank had a very fast airplane, clocked at 394.4 mph (635 kmh) in level flight, this cooling system was found to be problematic and the aircraft skin was prone to buckling and distortion.

The initial batch of three pre-production Fw 187 A-0 fighters were completed in the summer of 1939 with a rear facing radio/gunner position, and had 700 hp Jumo 210Ga engines. The armament consisted of two 0.787 in (20 mm) MG FF cannons and four 0.312 in (7.92 mm) MG 17 machine guns. The Luftwaffe had by this point decided that the rear defensive gun position of the aircraft was inadequate and unsuited for combat purposes. All three aircraft were returned to Focke-Wulf.

During the early months of 1940, several aircraft manufacturers formed a "Industrie-Schutzstaffel", in effect a private airforce to use as a point defence of their manufacturing plants to counter allied air attacks. Focke-Wulf used the three pre-production Fw 187 A-0 fighters at their plants and Heinkel used their nine pre-production He-100D-1 single seat fighters. Later the three Fw 187 A-0 aircraft were used as test beds for the Ta 154 program.

Fw 187 A-0 Ron Dupas Collection

Specifications (Fw 187 A-0)

Type:

Two-seat interceptor fighter

Engine:

Two 700 hp Jumo 210Ga twelve-cylinder four-stroke liquid-cooled inverted V-engines

Span:

50 ft 2.4 in (15.30 m)

Length:

36 ft 5.8 in (11.12 m)

Height:

12 ft 9.5 in (3.90 m)

Wing area:

327.23 sq.ft (30.40 sq.m)

Empty Wt:

8,157 lb (3,700 kg)

Max T/O Wt:

11,023 lb (5,000 kg)

Max speed:

322 mph (518 km/h) at 0 ft (0 m), 329 mph (530 km/h) at 13,780 ft (4,200 m)

Max climb:

3,445 ft (1,050 m)/min

Ceiling:

32,808 ft (10,000 m)

Models

Fw 187 V1/V2:

single-seat prototype; 680 hp Jumo 210Da engines: 2 built

Fw 187 V3/V5:

two-seated prototypes; cockpit and many detail changes: 3 built

Fw 187 V6:

as V3/V5; Daimler-Benz DB 600A engines; new coolant system: 1 built

Fw 187 A-0:

pre-production; Jumo 210Ga engines; new coolant system: 3 built