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Chyetverikov MDR 6

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Top speed
  
360 km/h

Length
  
16 m

Retired
  
1942

Manufacturer
  
OKB Chyetverikov

Wingspan
  
19 m

Introduced
  
1941

First flight
  
July 1937

Chyetverikov MDR-6 httpsuploadwikimediaorgwikipediacommonsdd

The Chyetverikov MDR-6 was a 1930s Soviet Union reconnaissance flying-boat aircraft, and the only successful aircraft designed by the design bureau led by Igor Chyetverikov.

Contents

Development

First flying in July 1937, the MDR-6 was a two-engined high-wing monoplane of all-metal stressed skin construction. The prototype was powered by two M-25 radial engines. A production run of 20 units powered by M-63 engines were produced in 1940 and 1941. All the aircraft were withdrawn from service in 1942 due to structural problems.

Several progressively advanced prototypes were built from 1939 to 1945, but no further production ensued.

Variants

MDR-6
Initial prototype. One built.
Chye-2
Production version powered by M-63 radial engine. 20 built.
MDR-6A
Redesign with smaller wing and two Klimov M-105 V-12 engines.
MDR-6B-1 to B-3
Refined developments of MDR-6A. Three prototypes built.
MDR-6B-4 to B5
New, much larger hull, powered by Klimov VK-107 engines. Two prototypes built.

Operators

 Soviet Union
  • Soviet Naval Aviation
  • Specifications (MDR-6A)

    Data from Donald, 1997, pg 258.

    General characteristics

  • Crew: 3
  • Capacity: 3
  • Length: 15.73 m (51 ft 7.25 in)
  • Wingspan: 19.4 m (63 ft 7.75 in)
  • Wing area: 52.3 m2 (562.97 ft2)
  • Empty weight: 4,100 kg (9,039 lb)
  • Gross weight: 7,200 kg (15,873 lb)
  • Powerplant: 2 × Shvetsov M-63 radial piston, 821 kW (1,100 hp) each each
  • Performance

  • Maximum speed: 360 km/h (224 mph)
  • Cruising speed: 220 km/h (137 mph)
  • Range: 2,650 km (1,647 miles)
  • Service ceiling: 9,000 m (29,530 ft)
  • Armament

  • 1 × 7.62-mm (0.3-in) ShKAS machine gun in bow turret
  • 1 × 12.7-mm (0.5-in) UBT machine gun in dorsal turret
  • 1,000-kg (2205-lb) bombload
  • References

    Chyetverikov MDR-6 Wikipedia


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