Shavrov Sh-3
From Wikipedia, the free encyclopedia
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
Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
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