Shavrov Sh-3

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The Shavrov Sh-3 was a Soviet project for a single-engined light amphibious aircraft designed by Vadim Shavrov for the transport role.[1] The programme was abandoned as the prototype was nearing completion.[1]

Specifications

General characteristics

  • Length: 7.80 m (36 ft 7 in)
  • Wingspan: 14.00 m (46 ft 11 in)
  • Wing area: 24 m2 (258.33 ft2)
  • Empty weight: 720 kg (1587 lb)
  • Gross weight: 1070 kg (2359 lb)
  • Powerplant: 1 × Cirrus Hermes, 89 kW (120 hp)

See also


Related lists

References

Notes

  1. 1.0 1.1 Orbis 1985, p. 2900

Bibliography

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