The Focke-Wulf Fw 187 Falke (Falcon)... was developed as a high-performance fight in the late 1930s. Designed by Kurt tank was also behind designing the beautiful looking Fw 200 Condor. The Luftwaffe in the end did not feel it fitted in with what they wanted and in the end only nine were built.
It first flew in May 1937. One and two seat prototypes we built. It suffered with trouble during development. One aircraft crashed after stalling, a couple crashed on landing and after an engine fire. Operationally three were used to defend of F-W’s factory. Another three were used in Norway, and one was used in Denmark. Pilots reported it was as good if not better than the Bf 110! It certainly looked better.
Specifications for the production Fw 187 A-0
It first flew in May 1937. One and two seat prototypes we built. It suffered with trouble during development. One aircraft crashed after stalling, a couple crashed on landing and after an engine fire. Operationally three were used to defend of F-W’s factory. Another three were used in Norway, and one was used in Denmark. Pilots reported it was as good if not better than the Bf 110! It certainly looked better.
Specifications for the production Fw 187 A-0
General characteristics:
Crew: 2
Length: 11.12 m (36 ft 6 in)
Wingspan: 15.30 m (50 ft 2 ? in)
Height: 3.85 m (12 ft 7 ? in)
Wing area: 30.40 m (327.22 ft²)
Empty weight: 3,700 kg (8,157 lb)
Loaded weight: 5,000 kg (11,023 lb)
Powerplant: 2 × Junkers Jumo 210G 12-cylinder inverted-V piston, 515 kW (700 PS) each
Crew: 2
Length: 11.12 m (36 ft 6 in)
Wingspan: 15.30 m (50 ft 2 ? in)
Height: 3.85 m (12 ft 7 ? in)
Wing area: 30.40 m (327.22 ft²)
Empty weight: 3,700 kg (8,157 lb)
Loaded weight: 5,000 kg (11,023 lb)
Powerplant: 2 × Junkers Jumo 210G 12-cylinder inverted-V piston, 515 kW (700 PS) each
Performance:
Maximum speed: 529 km/h at 4,200 m (329 mph at 13,780 ft)
Service ceiling: 10,000 m (32,810 ft)
Rate of climb: 1,050 m/min (3,445 ft/min)
Wing loading: 164.14 kg/m (33.62 lb/ft)
Maximum speed: 529 km/h at 4,200 m (329 mph at 13,780 ft)
Service ceiling: 10,000 m (32,810 ft)
Rate of climb: 1,050 m/min (3,445 ft/min)
Wing loading: 164.14 kg/m (33.62 lb/ft)
Armament:
4 × 7.92 mm (.312 in) MG 17 machine guns in fuselage sides
2 × 20 mm MG FF cannon in lower fuselage
4 × 7.92 mm (.312 in) MG 17 machine guns in fuselage sides
2 × 20 mm MG FF cannon in lower fuselage
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