Shavrov Sh-5
1934
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Shavrov Sh-5

The Sh-5 was developed for the purpose of aerial mapping. The first prototype flew on 19 March 1934. Project was cancelled by the end of the year with only one prototype built.

3-View 
Shavrov Sh-5A three-view drawing (800 x 540)


Specification 
 ENGINE2 x M-22, 480hp
 WEIGHTS
    Take-off weight5000 kg11023 lb
    Empty weight3470 kg7650 lb
 DIMENSIONS
    Wingspan24.0 m79 ft 9 in
    Length15.0 m49 ft 3 in
    Height6.2 m20 ft 4 in
    Wing area73.2 m2787.92 sq ft
 PERFORMANCE
    Max. speed213 km/h132 mph
    Ceiling4900 m16100 ft
    Range800 km497 miles

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