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| 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.
 | A three-view drawing (800 x 540) |
| ENGINE | 2 x M-22, 480hp |
| WEIGHTS |
| Take-off weight | 5000 kg | 11023 lb |
| Empty weight | 3470 kg | 7650 lb |
| DIMENSIONS |
| Wingspan | 24.0 m | 79 ft 9 in |
| Length | 15.0 m | 49 ft 3 in |
| Height | 6.2 m | 20 ft 4 in |
| Wing area | 73.2 m2 | 787.92 sq ft |
| PERFORMANCE |
| Max. speed | 213 km/h | 132 mph |
| Ceiling | 4900 m | 16100 ft |
| Range | 800 km | 497 miles |
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All the World's Rotorcraft |
