Ilyushin Il-6

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The Ilyushin Il-6 was a Soviet long-range bomber and torpedo bomber, designed as a replacement to the Il-4 for Soviet naval aviation. It strongly resembled its predecessor, but was larger, had pressurised crew accommodation for high-level operations, considerable sweepback on the wing leading edge and was powered by Charomsky ACh-30B engines.

Tests with the original Charomsky ACh-30B engines began at the factory on August 7 1943, with V.K. Kokkinaki at the controls, and were then continued at LII by test pilots A.N. Grinchik and N.S. Rybko.

In summer 1944, the more powerful ACh-30BF motors were installed, but continuing problems with the powerplants led to the cancellation of the whole project, with only a handful being built.

[edit] Specifications (Il-6)

[edit] General characteristics

  • Crew: three
  • Length: 17.38 m (57 ft 0 in)
  • Wingspan: 26.07 m (85 ft 6 in)
  • Height: 4.20 m (13 ft 9 in)
  • Wing area: 84.8 m² (913 ft²)
  • Empty: 11,830 kg (26,080 lb)
  • Loaded: 16,100 kg (35,500 lb)
  • Maximum takeoff: kg ( lb)
  • Powerplant: 2x Charomsky ACh-30BF inline diesels, 1,400 kW (1,900 hp) each

[edit] Performance

  • Maximum speed: 464 km/h (288 mph)
  • Range: 5,450 km (3,390 mi)
  • Service ceiling: 7,000 m (23,000 ft)
  • Rate of climb: 174 m/min (570 ft/min)
  • Wing loading: 190 kg/m² (39 lb/ft²)
  • Power/Mass: 0.18 kW/kg (0.11 hp/lb)

[edit] Armament

[edit] External links

[edit] Related content

Related development: Ilyushin Il-4

Comparable aircraft:

Designation sequence: Il-1 - Il-2 - Il-4 - Il-6 - Il-8 - Il-10 - Il-11


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